> Verlagsreihe
-
3310:
Further experimental investigations of the characteristics of cambered gothic wings at Mach numbers from 0'4 to 2'0 by L. C. Squire
London: H. M. Stationery Office, 1963
-
3279:
On the design of wing body combinations of low zero lift drag rise at transonic speeds by W. T. Lord
London: H. M. Stationery Office, 1962
-
3193:
Charts of peak amplitudes in incidence and sideslip in rolling manoeuvres due to inertia cross coupling by W. J. G. Pinsker
London: H. M. Stationery Office, 1962
-
3311:
NPL aerofoil catalogue and bibliography by R. C. Pankhurst
London: H. M. Stationery Office, 1962 [erschienen] 1963
-
3317:
Measurements of free stream turbulence in some low speed tunnels at NPL by P. Bradshaw and D. H. Ferriss
London: HMSO, 1962 [erschienen] 1963
-
3265:
On the flow in a reflected shock tunnel by D. W. Holder and D. L. Schultz
London: H. M. Stationery Office, [1962]
-
3322:
Upwash interference in a rectangular wind tunnel with closed side walls and porous slotted floor and roof by D. R. Holder
London: H. M. Stationery Office, 1962 [erschienen] 1963
-
3266:
Stresses produced in an infinite elastic plate by the application of loads travelling with uniform velocity along the bounding surfaces by L. S. D. Morley
London: H. M. Stationery Office, 1962
-
3301:
The use of a deep electrolytic tank as a lifting-surface calculator by H. S. Ward
London: H. M. Stationery Office, 1961 [erschienen] 1962
-
3302:
Some mathematical methods in three-dimensional subsonic flutter derivative theory D. E. Williams
London: H. M. Stationery Office, 1961 [erschienen] 1962
-
3304:
The aerodynamics of jet flaps J. Williams; S. F. J. Butler and M. N. Wood
London: H. M. Stationery Office, 1961 [erschienen] 1963
-
3283:
On the flexure of thin built up wings by G. G. Pope
London: H.M. Stationery Office, 1961 [erschienen] 1962
-
3262:
Interactions between normal shock waves and turbulent boundary layers by G. E. Gadd
London: HMSO, 1961 [erschienen] 1962
-
3209:
An experimental investigation of the transonic flow over an unswept wing of aspect ratio 3.5, taper ratio 0.5, with a 4 per cent biconvex section by J. B. Scott-Wilson
London: H. M. Stationery Office, 1961
-
3287:
A comparison of results in the A.R.A transonic tunnel on a small and a large model of a slender wing by T. E. B. Bateman and A. B. Haines
London: H. M. Stationery Office, 1961 [erschienen] 1962
-
3150:
Published reports and memoranda of the Aeronautical Research Council
London: H. M. Stationery Office, 1961
-
3160:
Some measurements on a yawed slender delta wing with leading-edge separation by J. K. Harvey
London: H.M. Stationery Office, 1961
-
3294:
Measurement of the pitching moment derivatives for rigid tapered wings of hexagonal planform oscillating in supersonic flow by L. Woodgate; J. F. M. Maybrey and C. Scruton
London: H. M. Stationery Office, 1961 [erschienen] 1962
-
3307:
Aerodynamic derivative measurements on a wing with horn balanced control surface by P. R. Guyett and J. K. Curran
London: H. M. Stationery Office, 1961 [erschienen] 1963
-
3306:
Experiments at M = 14̓1 on a thin, conically cambered elliptic cone of 30° semi vertex angle by E. W. E. Rogers, V. G. Quincey and J. Callinan
London: H. M. Stationery Office, 1961 [erschienen] 1963
-
3309:
The buckling of plates tapered in thickness by G. G. Pope
London: HMSO, 1961 [erschienen] 1963
-
3315:
Measurements of pitching moment derivatives for blunt nosed aerofoils oscillating in two dimensional supersonic flow by P. G. Pugh and L. Woodgate
London: H. M. Stationery Office, 1961 [erschienen] 1963
-
3146:
A method of calculating the velocity distribution on annular aerofoils in incompressible flow by J. A. Bagley; N. B. Kirby; P. J. Marcer
London: Her Majesty's Stationery Office, 1961
-
3308:
A numerical solution of an integral equation satisfied by the velocity distribution around a body of revolution in axial flow by D. Kershaw
London: H. M. Stationery Office, 1961 [erschienen] 1963
-
3281:
An experimental investigation of the structure of a leading edge vortex by P. B. Earnshaw
London: H. M. Stationery Office, 1961 [erschienen] 1962
-
3300:
Heat transfer through a constant-property laminar boundary layer by N. Curle
London: H. M. Stationery Office, 1961 [erschienen] 1962
-
3299:
The aerodynamic forces on an oscillating two-dimensional wing in accelerated supersonic flight by D. E. Davies
London: H. M. Stationery Office, 1961 [erschienen] 1962
-
3282:
The bursting of leading edge vortices - some observations and discussion of the phenomenon by N. C. Lambourne and D. W. Bryer
London: H.M. Stationery Office, 1961 [erschienen] 1962
-
3295:
The leading-edge buckling of a thin built-up wing due to aerodynamic heating by K. I. McKenzie
London: H. M. Stationery Office, 1961 [erschienen] 1962
-
3297:
Note on the evaluation of solid blockage corrections for rectangular wind tunnels with slotted walls by W. E. A. Acum
London: H. M. Stationery Office, 1961 [erschienen] 1962
-
3267:
The effect of temperature variations in the plane and through the thickness of a circular lenticular plate by E. H. Mansfield
London: H. M. Stationery Office, 1962
-
3280:
Measurement of aerodynamic heating on the nose of a delta aircraft at speeds up to M = 1,65 by J. E. Nethaway and O. P. Nicholas
London: H. M. Stationery Office, 1960 [erschienen] 1962
-
3050:
Published reports and memoranda of the Aeronautical Research Council
London: H. M. Stationery Office, 1960
-
3249:
Properties of a two-parameter family of thin conically cambered delta wings by slender body theory by J. C. Cooke
London: HMSO, 1960 [erschienen] 1962
-
3253:
The analysis of blade vibration due to random excitation by D. S. Whitehead
London: HMSO, 1960 [erschienen] 1962
-
3244:
Pressure distribution and surface flow on 5 % and 9 % thick wings with curved tip and 60° sweepback by H. C. Garner and D. E. Walshe
London: HMSO, 1960 [erschienen] 1962
-
3216:
The relationship between the discrete gust and power spectra presentations of atmospheric turbulence, with a suggested model of low altitude turbulence by J. K. Zbrozek
London: HMSO, 1960 [erschienen] 1961
-
3274:
Free-flight measurements of the transonic roll-damping characteristics of three related wings of aspect ratio 2.83 by K. J. Turner and G. K. Hunt
London: H. M. Stationery Office, 1960 [erschienen] 1962
-
3248:
Behaviour of skin fatigue cracks at the corners of windows in a Comet I fuselage by R. J. Atkinson; W. J. Winkworth and G. M. Norris
London: HMSO, 1960 [erschienen] 1962
-
3240:
The flow past a pitot tube at low Reynolds numbers by W. G. S. Lester
London: HMSO, 1960 [erschienen] 1961
-
3218:
Effects of heat transfer on laminar boundary layer development under pressure gradients in compressible flow by R. J. Monaghan
London: HMSO, 1960 [erschienen] 1961
-
3246:
An experimental investigation of heat transfer from the inside surface of a hot smooth tube to air, helium and carbon dioxide by J. F. Barnes
London: HMSO, 1960 [erschienen] 1961
-
3275:
Theory and tunnel tests of rotor blades for supersonic turbines by B. S. Stratford and G. E. Sansome
London: H. M. Stationery Office, 1960 [erschienen] 1962
-
3259:
A narrow band spectral analyser for random waveforms by D. S. Whitehead
London: HMSO, 1960 [erschienen] 1962
-
3228:
Performance of the 36 x 35 in. slotted transonic working section of the R.A.E. Bedford 3-ft wind tunnel by E. P. Sutton, M. T. Caiger and A. Stanbrook
London: HMSO, 1960 [erschienen] 1961
-
3223:
The longitudinal stability and control of the tandem rotor helicopter by A. R. S. Bramwell
London: HMSO, 1960 [erschienen] 1961
-
3237:
The hemispherical, differential pressure yawmeter at supersonic speed by L. J. Beecham
London: HMSO, 1960 [erschienen] 1961
-
3245:
Thermal buckling of circular plates by B. Cotterell and E. W. Parkes
London: HMSO, 1960 [erschienen] 1962
-
3270:
A study of the effect of leading edge modifications on the flow over a 50-deg sweptback wing at transonic speeds by E. W. E. Rogers; C. J. Berry and J. E. G. Townsend
London: H. M. Stationery Office, 1960 [erschienen] 1962
-
3271:
The flow pattern on a tapered sweptback wing at mach numbers between 0.6 and 1.6 (part 1)
London: H. M. Stationery Office, 1960 [erschienen] 1962
-
3139:
A method for calculating the pressure distribution of a body of revolution moving in a circular path through a perfect incompressible fluid by F. Vandrey
London: Her Majesty's Stationery Office, 1960
-
3236:
Thermal stresses near the roots of rectangular wings by G. G. Pope
London: HMSO, 1960 [erschienen] 1961
-
3238:
The pressure distribution on two-dimensional wings near the ground by J. A. Bagley
London: HMSO, 1960 [erschienen] 1961
-
3239:
Some convergence problems in the numerical solution of the Navier Stokes equations by W. G. S. Lester
London: HMSO, 1960 [erschienen] 1961
-
3243:
Flight tests to investigate the dynamic lateral stability characteristics of a 45-deg delta, cropped to give three aspect ratios by J. E. Nethaway and J. Clark
London: HMSO, 1960 [erschienen] 1962
-
3278:
Some applications of 'not-so-slender' wing theory to wings with curved leading edges by L. C. Squire
London: H. M. Stationery Office, 1960 [erschienen] 1962
-
3254:
Force and moment coefficients for vibrating aerofoils in cascade by D. S. Whitehead
London: HMSO, 1960 [erschienen] 1962
-
3256:
A note on flutter of asymmetric controls by E. G. Broadbent and E. V. Hartley
London: HMSO, 1960 [erschienen] 1962
-
3142:
Aerodynamic characteristics of rectangular wings of small aspect ratio by I. J. Campbell; C. F. Blanks and D. A. Leaver
London: H.M. Stationery Office, 1960
-
3213:
Abstracts of papers published externally
London: HMSO, 1960
-
3252:
Turbulent wall jets with and without an external stream by P. Bradshaw and M. T. Gee
London: HMSO, 1960 [erschienen] 1962
-
3145:
Wind-tunnel tests on the use of distributed suction for maintaining laminar flow on a body of revolution by N. Gregory; W. S. Walker
London: Her Majesty's Stationery Office, 1960
-
3298:
Calculation of stability derivatives for tapered wings of hexagonal planform oscillating in a supersonic stream by Doris E. Lehrian
London: H. M. Stationery Office, 1960 [erschienen] 1963
-
3288:
Experiments on a delta wing with jet assisted lift by W. H. Melbourne
London: H. M. Stationery Office, 1960 [erschienen] 1962
-
3143:
The effect of changes in the stability derivatives on the dynamic behaviour of a torpedo by J. D. Lambert
London: Her Majesty's Stationery Office, 1960
-
3111:
Note on the lift slope, and some other properties, of delta and swept back wings by E. F. Relf
London: H. M. Stationery Office, 1959
-
3292:
Further results on the mixing of free axially symmetrical jets of Mach number 1.40 by N. H. Johannesen
London: H. M. Stationery Office, 1959 [erschienen] 1962
-
3200:
An axially symmetric analogue for general three-dimensional boundary layers by J. C. Cooke
London: H. M. Stationery Office, 1959 [erschienen] 1961
-
3224:
The effect of a central jet on the base pressure of a cylindrical after-body in a supersonic stream by J. Reid and R. C. Hastings
London: HMSO, 1959 [erschienen] 1961
-
3229:
The velocity potential on triangular and related wings with subsonic leading edges oscillating harmonically in supersonic flow by D. E. Davies
London: HMSO, 1959 [erschienen] 1961
-
3232:
A record of information on oscillatory aerodynamic derivative measurements by H. Hall
London: HMSO, 1959 [erschienen] 1962
-
3235:
On axi-symmetrical gas jets, with application to rocket jet flow fields at high altitudes by W. T. Lord
London: HMSO, 1959 [erschienen] 1962
-
3215:
The effect of humidity on laminar recovery temperature measurements in supersonic flow of air in wind tunnels by J. F. W. Crane
London: HMSO, 1959 [erschienen] 1961
-
3099:
Thermodynamic data for the calculation of gas turbine performance by D. Fielding and J. E. C. Topps
London: Her Majestys's Stationery Office, 1959
-
3273:
The performance of supersonic turbine nozzles by B. S. Stratford and G. E. Sansome
London: H. M. Stationery Office, 1959 [erschienen] 1962
-
3268:
Effects of wing stiffness and inertia changes on the modes and frequencies of a model delta aircraft by D. R. B. Webb
London: H. M. Stationery Office, 1959 [erschienen] 1962
-
3191:
The growth of compressible turbulent boundary layers on isothermal and adiabatic walls by D. A. Spence
London: H. M. Stationery Office, 1959 [erschienen] 1961
-
3207:
The calculation of the compressible turbulent boundary layer in an arbitrary pressure gradient a correlation of certain previous methods by B. S. Stratford and G. S. Beavers
London: H. M. Stationery Office, 1959 [erschienen] 1961
-
3202:
The determination of local turbulent skin friction from observations in the viscous sub-layer by P. Bradshaw and N. Gregory
London: H. M. Stationery Office, 1959 [erschienen] 1961
-
3219:
The interference on a three-dimensional jet flap wing in a closed wind tunnel by E. C. Maskell
London: HMSO, 1959 [erschienen] 1961
-
3222:
Some notes on the zero-lift wave drag of slender wings with unswept trailing edge by J. Weber
London: HMSO, 1959 [erschienen] 1961
-
3242:
The test performance of highly loaded turbine stages designed for high pressure ratio by I. H. Johnston and D. C. Dransfield
London: HMSO, 1959 [erschienen] 1962
-
3211:
An experimental investigation at supersonic speeds of the characteristics of two gothic wings, one plane and one cambered by L. C. Squire
London: HMSO, 1959 [erschienen] 1961
-
3214:
Theoretical subsonic derivatives for an oscillating M-wing by H. C. Garner and W. E. A. Acum
London: HMSO, 1959 [erschienen] 1961
-
3217:
Formulae for calculating the camber surfaces of thin swept back wings of arbitrary plan form with subsonic leading edges, and specified load distribution by G. M. Roper
London: HMSO, 1959 [erschienen] 1961
-
3118:
Experiments on distributed suction through a rough porous surface by The Cambridge University Aeronautical Laboratory
London: Her Majesty's Stationery Office, 1959
-
3133:
Boundary layer measurements on 15-deg and 24.5-deg cones at small angles of incidence at M3.17 and 3.82 and zero heat transfer by F. V. Davies and R. J. Monaghan
London: H. M. Stationery Office, 1959 [erschienen] 1960
-
3201:
Approximate calculation of three-dimensional laminar boundary layers by J. C. Cooke
London: H. M. Stationery Office, 1959 [erschienen] 1961
-
3226:
A wind tunnel investigation of the longitudinal and lateral aerodynamic characteristics of a canard aircraft model by P. E. Watts and L. J. Beecham. D. A. Treadgold
London: HMSO, 1959 [erschienen] 1962
-
3227:
A theoretical study of annular supersonic nozzles by W. T. Lord
London: H. M. Stationery Office, 1959 [erschienen] 1961
-
3234:
Measurement of pitching moment derivatives for aerofoils oscillating in two-dimensional supersonic flow by C. Scruton
London: HMSO, 1959 [erschienen] 1962
-
3260:
A proposed apparatus for measuring oscillatory aerodynamic derivatives by L. H. G. Sterne
London: HMSO, 1959 [erschienen] 1962
-
3132:
Drag reduction of thin wings at supersonic speeds, by the use of camber and twist by G. M. Roper
London: H. M. Stationery Office, 1959 [erschienen] 1960
-
3205:
The normal impingement of a circular air jet on a flat surface by P. Bradshaw and Edna M. Love
London: H. M. Stationery Office, 1959 [erschienen] 1961
-
3221:
Numerical methods for calculating the zero-lift wave drag and the lift dependent wave drag of slender wings by J. Weber
London: HMSO, 1959 [erschienen] 1961
-
3247:
A description of the excitation and recording equipment used for flight flutter tests an a Meteor 8 by P. D. R. Luscombe
London: HMSO, 1959 [erschienen] 1962
-
3187:
Calculation of flexible wall shapes and preparation of control tapes for the bedford 8-ft x 8-ft wind tunnel by Marjorie M. Barritt
London: H. M. Stationery Office, 1959 [erschienen] 1961
-
3173:
Wave theory of the Mach-Zehnder interferometer by H. K. Zienkiewicz
London: HMSO, 1959 [erschienen] 1961
-
3276:
Principles of attitude control of artificial satellites by N. E. Ives
London: H. M. Stationery Office, 1959 [erschienen] 1962
-
3264:
Wind tunnel tests and theoretical investigations on the effect of a localised mass on the flutter of a delta wing with fixed root by G. F. Donno
London: HM Stationery Office, 1959 [erschienen] 1962
-
3258:
Some possible effects of transonic speeds on wing-aileron flutter by E. G. Broadbent and E. Violet Hartley
London: Her Majesty's Stationery Office, 1959 [erschienen] 1962
-
3180:
Observations of the flow over a two-dimensional 4 per cent thick aerofoil at transonic speeds by B. D. Henshall and R. F. Cash
London: H. M. Stationery Office, 1959 [erschienen] 1961
-
2982:
Thermodynamic charts for the combustion products of nitric acid and kerosene by W. H. Williams
London: HMSO, 1959
-
3198:
The buckling of a pressurised stiffened cylinder under axial load by K. I. McKenzie
London: H. M. Stationery Office, 1959 [erschienen] 1961
-
3197:
Leading edge buckling due to aerodynamic heating by E. H. Mansfield
London: H. M. Stationery Office, 1959 [erschienen] 1960
-
3277:
The calculation of the rotary lateral stability derivatives of a jet flapped wing by H. H. B. M. Thomas
London: HMSO, 1958 [erschienen] 1962
-
3290:
Free flight measurements of pressure distribution at transonic and supersonic speeds on bodies of revolution having parabolic afterbodies by C. Kell
London: H. M. Stationery Office, 1958 [erschienen] 1962
-
3176:
An investigation at low speed of the flow near the apex of thin delta wings with sharp leading edges by B. J. Elle
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3089:
Some factors influencing the speed of response of hydraulic position servomechanics by C. W. Lewis
London: H. M. Stationery Office, 1958
-
3091:
An experimental investigation of leading-edge flow separation from a 4 per cent thick two-dimensional biconvex aerofoil by B. D. Henshall; R. F. Cash
London: Her Majesty's Stationery Office, 1958
-
3074:
Flow in a jet directed normal to the wind by R. Jordinson
London: Her Majesty's Stationery Office, 1958
-
3037:
Pressure probes selected for three-dimensional flow measurement by D. W. Bryer and H. C. Garner
London: H. M. Stationery Office, 1958
-
3152:
Entrainment in the turbulent boundary layer by M. R. Head
London: Her Majesty's Stationery Office, 1958 [erschienen] 1960
-
3178:
The stability of rotor blade flapping motion by A. G. Shutler and J. P. Jones
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3066:
The effect of inlet circumferential maldistribution on an axial compressor stage by R. C. Turner, J. Ritchie and C. E. Moss
London: H. M. Stationery Office, 1958
-
3046:
The influence of plain bearings on shaft whirling by E. Downham
London: H. M. Stationery Office, 1958
-
3285:
Seaplane impact - a review of theoretical and experimental results by T. Arlotte; P. Ward Brown and P. R. Crewe
London: H. M. Stationery Office, 1958 [erschienen] 1962
-
3196:
Use of camber and twist to produce low drag delta or swept back wings, without leading edge singularities, at supersonic speeds by G. M. Roper
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3194:
An analysis of the flow over two 45-deg swept back wings at high subsonic speeds, and comparison with theory by R. Cook
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3225:
Measurement of the performance of a single stage, high mach number, subsonic axial flow compressor by R. Staniforth
London: HMSO, 1958 [erschienen] 1961
-
3156:
Review and extension of transonic aerofoil theory parts 1 to 3 by C. S. Sinnott and J. Osborne
London: H.M. Stationery Office, 1958 [erschienen] 1961
-
3106:
Some visual observations of the effects of sweep on the low speed flow over a sharp edged plate at incidence by N. C. Lambourne and P. S. Pusey
London: H. M. Stationery Office, 1958 [erschienen] 1959
-
3119:
The theoretical evaluation of the downwash behind jet flapped wings by A. J. Ross
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3185:
On the measurement of local surface friction on a flat plate by means of preston tubes
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3203:
An experimental method for the study of the impact between a liquid drop and a surface moving at high speed by D. C. Jenkins, J. D. Booker and J. W. Sweed
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3199:
A calculation method for three-dimensional turbulent boundary layers by J. C. Cooke
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3220:
Tests on an experimental three stage turbine fitted with low reaction blading of unconventional form by I. H. Johnston and G. E. Sansome
London: HMSO, 1958 [erschienen] 1961
-
3212:
A supersonic tunnel design for testing engine intakes by R. Staniforth
London: HMSO, 1958 [erschienen] 1961
-
3159:
Explanation of poorly damped lateral oscillations during automatic approach with aileron steering by K. H. Doetsch
London: Her Majesty's Stationery Office, 1958 [erschienen] 1960
-
3135:
The properties of a thin conically cambered wing according to slender body theory by J. H. B. Smith
London: H. M. Stationery Office, 1958 [erschienen] 1960
-
3137:
The calculation of lift slopes, allowing for boundary layer, with applications to the RAE 101 and 104 aerofoils by D. A. Spence and J. A. Beasley
London: H. M. Stationery Office, 1958 [erschienen] 1960
-
3181:
Blade vibratory stresses in a multi-stage axial flow compressor by D. A. Kilpatrick, A. D. S. Carter and L. O'Neill
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3230:
10-ft x 7-ft tunnel tests up to M0.94 of nose droop and a blunt nosed NACA 3-00 type section on a 7 1/2 per cent thick 50 deg swept wing by A. L. Courtney
London: HMSO, 1958 [erschienen] 1961
-
3167:
Flexible mass balance arms and control surface flutter by D. Moxon
London: Her Majesty's Stationery Office, 1958 [erschienen] 1960
-
3162:
Pressure fluctuations near a cold, small scale air jet (measurement of space correlations) by R. E. Franklin and J. H. Foxwell
London: H.M. Stationery Office, 1958 [erschienen] 1960
-
3193:
A free flight investigation into the effect of body shaping on the zero-lift drag of a wing body combination at transonic and supersonic speeds by J. A. Hamilton, G. H. Greenwood and W. T. Lord
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3251:
An analysis of some VTOL transition motions by S. B. Gates and C. F. Griggs
London: HMSO, 1958 [erschienen] 1962
-
3255:
Wind tunnel tests on the effects of an added mass on the flutter of a model delta wing by H. Hall and W. A. Coles
London: HMSO, 1958 [erschienen] 1962
-
3148:
Heat transfer and skin friction measurements at a Mach number of 2.44 for a turbulent boundary layer on a flat surface and in regions of separated flow by G. E. Gadd, W. F. Cope and J. L. Attridge
London: H.M. Stationery Office, 1958 [erschienen] 1960
-
3147:
A note on the theory of the Stanton tube by G. E. Gadd
London: H.M. Stationery Office, 1958 [erschienen] 1960
-
3161:
Correlation in the random pressure field close to a jet by R. E. Franklin and J. H. Foxwell
London: H.M. Stationery Office, 1958 [erschienen] 1960
-
3186:
Low speed wind tunnel tests on a series of uncambered slender pointed wings with sharp edges by D. H. Peckham
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3158:
Thermodynamic charts for the decomposition products of 80, 85 and 90 per cent w w hydrogen peroxide (H.T.P.) by Enid Carter
London: H. M. Stationery Office, 1958 [erschienen] 1960
-
3171:
Aerodynamic derivative measurements on a rectangular wing of aspect ratio 3.3 by P. R. Guyett and J. K. Curran
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3168:
The effects of various parameters on wing torsion aileron rotation flutter by A. D. N. Smith
London: HMSO, 1958 [erschienen] 1960
-
2950:
Published reports and memoranda of the Aeronautical Research Council
London: [H. M. Stationery Office], [1958]
-
3313:
Tests on the loss of vertical jet thrust due to ground effect on two simple VTOL planforms, with particular reference to the short SC1 aircraft by L. A. Wyatt
London: H. M. Stationery Office, 1958 [erschienen] 1963
-
3314:
The stability of an aircraft under automatic throttle control and the cross coupling effects with elevator control by D. E. Fry and M. R. Watts
London: H. M. Stationery Office, 1958 [erschienen] 1963
-
3177:
The torsional oscillations of airscrew blades at low mean incidences by J. P. Jones
London: HMSO, 1958 [erschienen] 1960
-
3296:
A preliminary data report on ground pressure disturbances produced by the Fairey Delta 2 in level supersonic flight by T. A. Holbeche
London: H. M. Stationery Office, 1958 [erschienen] 1963
-
3172:
The hydro-elastic stability of hydrofoil struts by D. V. Hilborne
London: H. M. Stationery Office, 1958 [erschienen] 1960
-
3263:
Measurements of lift and ground interference on a lifting fan wing at zero forward speed by N. Gregory and W. S. Walker
London: H.M. Stationery Office, 1958 [erschienen] 1962
-
3140:
The centre line mach number distributions and auxiliary suction requirements for the A.R.A. 9-ft x 8-ft transonic wind tunnel by A. B. Haines and J. C. M. Jones
London: H. M. Stationery Office, 1958 [erschienen] 1960
-
3126:
Notes on the derivation of true air temperature from aircraft observations by D. D. Clark
London: H. M. Stationery Office, 1958 [erschienen] 1960
-
3179:
Heat transfer and laminar boundary layer separation in steady compressible flow past a wall with non-uniform temperature by N. Curle
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3155:
The effects of distributed suction on the development of turbulent boundary layers by R. A. Dutton
London: H. M. Stationery Office, 1958 [erschienen] 1960
-
3164:
Accurate solutions of the laminar boundary layer equations, for flows having a stagnation point and separation by N. Curle
London: H. M. Stationery Office, 1958 [erschienen] 1960
-
3153:
An improved strain gauge type of load cell thrust transducer by D. S. Dean
London: Her Majesty's Stationery Office, 1958 [erschienen] 1960
-
3125:
Vectorial analysis of flight flutter test results by E. G. Broadbent and E. Violet Hartley
London: Her Majesty's Stationery Office, 1958 [erschienen] 1961
-
2850:
Published reports and memoranda of the Aeronautical Research Council [(Nos. 2751 - 2850)]
London: HMSO, 1958
-
2882:
Low speed tests on 45 deg swept-back wings parts 1 and 2 by J. Weber, D. Küchemann and G. G. Brebner
London: HMSO, 1958
-
2970:
Gust alleviation factor by J. K. Zbrozek
London: HMSO, 1958
-
3149:
An analysis of the lateral directional stability and control of the single rotor helicopter by G. F. Langdon and M. C. Neale
London: H.M. Stationery Office, 1958 [erschienen] 1960
-
3136:
Secondary flow and losses in a compressor cascade by Jean F. Louis
London: H. M. Stationery Office, 1958 [erschienen] 1960
-
3175:
The steady flow of a viscous fluid past a circular cylinder at Reynolds numbers 40 and 44 by C. J. Apelt
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3195:
Combined flexure and torsion of a class of heated thin wings a large-deflection analysis by E. H. Mansfield
London: H. M. Stationery Office, 1958 [erschienen] 1961
-
3100:
Experiments with a two-dimensional aerofoil designed to be free from turbulent boundary layer separation at small angles of incidence for all mach numbers by D. W. Holder and R. F. Cash
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3031:
Experimental and theoretical investigations of the flow of air through two single stage compressors by J. H. Horlock
London: H. M. Stationery Office, 1957
-
3123:
An approximate method of calculating the laminar boundary layer in two-dimensional incompressible flow by M. R. Head
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3093:
Observations of the flow patterns of a two-dimensional 4 per cent thick biconvex aerofoil at M1̥4̓0 and 16̓3 by B. D. Henshall and R. F. Cash
London: H. M. Stationery Office, 1957 [erschienen] 1958
-
3291:
The mixing of free axially symmetrical jets of Mach number 1.40 by N. H. Johannesen
London: H. M. Stationery Office, 1957 [erschienen] 1962
-
3098:
The shape of the centre part of a swept back wing with a required load distribution by J. Weber
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3090:
The pressure in a two-dimensional static hole at low Reynolds numbers by A. Thom and C. J. Apelt
London: H. M. Stationery Office, 1957 [erschienen] 1958
-
3122:
The formation of regions of separated flow on wing surfaces by L. F. Crabtree
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3131:
The design and use of interferometers in aerodynamics by L. H. Tanner
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3128:
Experiments with inclined blunt nosed bodies at M 0 = 2.45 by I. M. Hall; E. W. E. Rogers and B. M. Davis
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3104:
Longitudinal stability and control of the single rotor helicopter by A. R. S. Bramwell
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3120:
Low speed experiments on the wake characteristics of flat plates normal to an air stream by R. Fail; J. A. Lawford and R. C. W. Eyre
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3121:
Investigations into the use of on electrical resistance analogue for the solution of certain oscillatory flow problems by P. J. Palmer; Anne R. Copson and S. C. Redshaw
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3076:
The wave drag of non-lifting combinations of thin wings and 'Non-Slender' bodies by L. M. Sheppard
London: HMSO, 1957 [erschienen] 1958
-
3077:
Methods for determining the wave drag of non-lifting wing body combinations by L. M. Sheppard
London: HMSO, 1957 [erschienen] 1958
-
3097:
The development of a variable Mach number effuser by J. B. McGarry
London: H. M. Stationery Office, 1957 [erschienen] 1958
-
3092:
Observations of the flow past a two-dimensional 4 per cent thick biconvex aerofoil at high subsonic speeds by B. D. Henshall and R. F. Cash
London: H. M. Stationery Office, 1957 [erschienen] 1958
-
3129:
Low speed wind tunnel tests on the De Havilland Sea Venom with blowing over the flaps by S. F. J. Butler and M. B. Guyett
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3189:
Body freedom flutter of ground launched rocket models at supersonic and high subsonic speeds by D. R. Gaukroger
London: H. M. Stationery Office, 1957 [erschienen] 1961
-
3034:
The matrix force method of structural analysis and some new applications by J. H. Argyris and S. Kelsey
London: H. M. Stationery Office, 1957
-
3116:
A theory of the separated flow from the curved leading edge of a slender wing by J. H. B. Smith
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3124:
Approximate calculations of the laminar boundary layer with suction, with particular reference to the suction requirements for boundary layer stability on aerofoils of different thickness-chord ratios by M. R. Head
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3134:
Subsonic wind tunnel tests of various forms of air intake installed in a fighter type aircraft by B. J. Prior and C. N. Hall
London: H. M. Stationery Office, 1957 [erschienen] 1960
-
3138:
Some exploratory jet flap tests on a 60-deg delta wing by J. Williams and A. J. Alexander
London: H. M. Stationery Office, 1957 [erschienen] 1961
-
3113:
Methods for estimating distributions and intensities of sonic bangs by D. G. Randall
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3115:
The influence of aerodynamic heating on the flexural rigidity of a thin wing by E. H. Mansfield
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3044:
On some aspects of the use of shock tubes in aerodynamic research by B. D. Henshall
London: H. M. Stationery Office, 1957
-
3289:
The use of conical camber to produce flow attachment at the leading edge of a delta wing and to minimize lift-dependent drag at sonic and supersonic speeds by J. H. B. Smith and K. W. Mangler
London: H. M. stationery Office, 1957 [erschienen] 1963
-
3269:
Concept of complex stiffness applied to problems of oscillations with viscous and hysteretic damping by S. Neumark
London: H. M. Stationery Office, 1957 [erschienen] 1962
-
3114:
Experimental observation of vortices in wing body junctions by A. Stanbrook
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3036:
A method for calculating the pressure distribution over jet-flapped wings by D. Küchemann
London: Her Majesty's Stationery Office, 1957
-
3107:
Experimental study of surface flow and part span vortex layers on a cropped arrowhead wing by H. C. Garner and D. W. Bryer
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
3183:
The design and testing of an axial flow compressor having different blade profiles in each stage by A. D. S. Carter
London: H. M. Stationery Office, 1957 [erschienen] 1960
-
3020:
An extension of the hydrodynamic source-sink method for ayisymmetric bodies by A. H. Armstrong
London: Her Majesty's Stationery Office, 1957
-
3026:
The calculation of the pressure distribution on the surface of thick cambered wings and the design of wings with given pressure distribution by J. Weber
London: Her Majesty's Stationery Office, 1957
-
2958:
An analysis of the longitudinal stability and control of a single rotor helicopter by F. O'Hara
London: HMSO, 1957
-
3105:
Aerodynamic characteristics in the approach, superfine and negative pitch ranges of two four bladed propellers with NACA Series 16 blade sections a report of tests carried out jointly by the technical staffs of de Havilland Propellers, Limited, and Rotol, Limited
London: H. M. Stationery Office, 1957 [erschienen] 1959
-
2961:
Calculation of flutter derivatives for wings of general plan form by Doris E. Lehrian
London: HMSO, 1957
-
2935:
A simple method for calculating the span and chordwise loading on straight and swept wings of any given aspect ratio at subsonic speeds by D. Küchemann
London: [H. M. Stationery Office], 1957
-
3174:
Charts for low speed characteristics of two-dimensional trailing edge flaps by H. C. Garner
London: Her Majesty's Stationery Office, 1957 [erschienen] 1960
-
3170:
The measurement of unsteady forces and moments on slender bodies oscillating in a wind tunnel by J. F. Clarke
London: H. M. Stationery Office, 1957 [erschienen] 1960
-
3184:
The effect of Reynolds number on the performance of a single stage compressor by A. D. S. Carter
London: H. M. Stationery Office, 1957 [erschienen] 1960
-
3163:
Measurements of the direct hinge moment derivatives at subsonic and transonic speeds for a cropped delta wing with oscillating flap by J. B. Bratt, C. J. W. Miles and R. F. Johnson
London: Her Majesty's Stationery Office, 1957 [erschienen] 1960
-
3284:
Flutter of an all-moving tailplane by E. G. Broadbent and Margaret Williams
London: Her Majesty's Stationery Office, 1957 [erschienen] 1962
-
3002:
Flow in the laminar boundary layer near separation by B. S. Stratford. With an app. by G. E. Gadd
London: HMSO, 1957
-
2889:
Theoretical load distribution on a wing with a cylindrical body at one end by J. Weber
London: Her Majesty's Stationery Office, 1957
-
2750:
Published reports and memoranda of the Aeronautical Research Council [(Nos. 2651 - 2750)]
London: HMSO, 1957
-
3006:
The three-dimensional boundary-layer equations and some power series solutions by L. C. Squire
London: Her Majesty's Stationery Office, 1957
-
2917:
Investigations of the behaviour of aircraft when making a forced landing on water (ditching) by A. G. Smith; C. H. E. Warren; D. F. Wright
London: Her Majesty's Stationery Office, 1957
-
2855:
Oscillating wings in compressible subsonic flow by W. P. Jones
London: HMSO, 1957
-
3182:
Vortex lattice treatment of rectangular wings with oscillating control surfaces by Doris E. Lehrian
London: H. M. Stationery Office, 1957 [erschienen] 1960
-
3154:
Free vibrations of a stiffened cylindrical shell by P. R. Miller
London: H. M. Stationery Office, 1957 [erschienen] 1960
-
3039:
The theoretical determination of normal modes and frequencies of vibration by I. T. Minhinnick
London: H. M. Stationery Office, 1956 [erschienen] 1957
-
3048:
A general method (depending on the aid of a digital computer) for deriving the structural influence coefficients of aeroplane wings by D. Williams
London: H. M. Stationery Office, 1956 [erschienen] 1959
-
3068:
Calculated derivatives for rectangular wings oscillating in compressible subsonic flow by Doris E. Lehrian
London: H. M. Stationery Office, 1956 [erschienen] 1958
-
3081:
Wind tunnel tests on the effect of body freedoms on the flutter of a model wing carrying a localised mass by D. R. Gaukroger and E. W. Chapple
London: H. M. Stationery Office, 1956 [erschienen] 1958
-
3082:
The full scale air drag of some flying boat seaplanes by A. G. Smith
London: H. M. Stationery Office, 1956 [erschienen] 1959
-
3080:
Supersonic wind tunnel flutter tests of two rectangular wings by P. R. Guyett
London: HMSO, 1956 [erschienen] 1958
-
3095:
An investigation or the hydrodynamic stability and spray characteristics of high length beam ratio seaplane hulls with beam loadings
London: HMSO, 1956 [erschienen] 1959
-
3055:
A theoretical and experimental investigation of the flow over a family of rectangular wings of biconvex section at M = 14̓2 by R. C. Lock
London: H. M. Stationery Office, 1956 [erschienen] 1958
-
3061:
Note on the convergence of numerical solutions of the Navier-Stokes equations by A. Thom and C. J. Apelt
London: H. M. Stationery Office, 1956 [erschienen] 1958
-
3087:
Pressure plotting measurements on an 8 per cent thick aerofoil with trailing edge flap blowing by J. Williams and A. J. Alexander
London: H. M. Stationery Office, 1956 [erschienen] 1958
-
3069:
The optics of the Mach-Zehnder interferometer by L. H. Tanner
London: H. M. Stat. Off., 1956 [erschienen] 1959
-
3047:
A numerical method for calculating the starting and perturbation of a two-dimensional jet at low Reynolds number by R. B. Payne
London: H. M. Stationery Office, 1956 [erschienen] 1958
-
3064:
Experiments on two-dimensional base flow at M = 2.4 by L. Fuller and J. Reid
London: H. M. Stationery Office, 1956 [erschienen] 1958
-
3058:
The accuracy of the measurement of turbulent skin friction by means of surface pitot tubes and the distribution of skin friction on a flat plate by R. A. Dutton
London: H. M. Stationery Office, 1956 [erschienen] 1957
-
3072:
The effect of wing torsion on aileron tab flutter by H. Hall
London: HMSO, 1956 [erschienen] 1958
-
3075:
Operational formulae for response calculations by S. Neumark
London: HMSO, 1956 [erschienen] 1958
-
3103:
Aspect ratio effects on compressor cascade blade flutter by D. A. Kilpatrick and R. A. Burrows
London: H. M. Stationery Office, 1956 [erschienen] 1958
-
3060:
Calculation of derivatives for a cropped delta wing with subsonic leading edges oscillating in a supersonic air stream by J. Watson
London: H. M. Stationery Office, 1956 [erschienen] 1958
-
3206:
Direct solution of the flutter problem by P. Lancaster
London: H. M. Stationery Office, 1956 [erschienen] 1961
-
3054:
On flutter testing in high-speed wind tunnels by N. C. Lambourne and C. Scruton
London: Her Majestys's Stationery Office, 1956 [erschienen] 1958
-
3204:
The effect of internal contraction, initial rate of subsonic diffusion, and cowl and centrebody shape on the pressure recovery of a conical centrebody intake at supersonic speeds by E. L. Goldsmith
London: H. M. Stationery Office, 1956 [erschienen] 1962
-
3051:
A subsonic lifting surface theory for low aspect ratio wings by C. R. Taylor
London: Her Majestys's Stationery Office, 1956 [erschienen] 1957
-
3053:
Some experiments with sonic throats downstream from the working section of a slotted wall high-speed tunnel by A. Chinneck and N. A. North
London: Her Majestys's Stationery Office, 1956 [erschienen] 1957
-
3166:
A note on test factors by N. I. Bullen
London: Her Majesty's Stationery Office, 1956 [erschienen] 1961
-
3063:
The sampling errors of atmospheric turbulence measurements by N. I. Bullen
London: Her Majestys's Stationery Office, 1956 [erschienen] 1958
-
2943:
Wind tunnel wall interference effects on oscillating aerofoils in subsonic flow by W. P. Jones
London: [Her Majestys's Stationery Office], [1956]
-
3028:
Experiments on pitot tubes in shear flow by F. A. MacMillan
London: H. M. Stationery Office, 1956 [erschienen] 1957
-
3169:
The effect of structural damping on binary flutter by E. G. Broadbent and Margaret Williams
London: Her Majesty's Stationery Office, 1956 [erschienen] 1960
-
2906:
The spinning of model aircraft and the prediction of full-scale spin and recovery characteristics by G. E. Pringle and D. J. Harper
London: H.M. Stat. Off., 1956
-
2908:
The subsonic flow past swept wings at zero lift without and with body by D. Küchemann; J. Weber
London: Her Majesty's Stationery Office, 1956
-
2968:
Wind-tunnel observations of boundary-layer transition on a wing at various angles of sweepback by A. Anscombe; L. N. Illingworth
London: Her Majesty's Stationery Office, 1956
-
2785:
Notes on the transonic movement of wing aerodynamic centre by S. B. Gates
London: HMSO, 1956
-
2980:
A study of the aircraft arresting hook bounce problem by J. Thomlinson
London: HMSO, 1956
-
3041:
The icing of compressor blades and their protection by surface heating by G. I. Shires and G. E. Munns
London: H. M. Stationery Office, 1955 [erschienen] 1958
-
3108:
Some effects of shock induced separation of turbulent boundary layers in transonic flow past aerofoils by H. H. Pearcey
London: H. M. Stationery Office, 1955 [erschienen] 1959
-
3071:
A comparison of the measured and predicted flutter characteristics of a series of delta wings of different aspect ratios by H. Hall and E. W. Chapple
London: H. M. Stationery Office, 1955 [erschienen] 1958
-
3059:
Calculation of derivatives for a cropped delta wing with an oscillating constant chord flap in a supersonic air stream by J. Watson
London: H. M. Stationery Office, 1955 [erschienen] 1958
-
3018:
Wind tunnel tests on seaplane hulls in the R.A.E. 5-ft. diameter open jet tunnel and the N.P.L. compressed air tunnel by A. G. Smith
London: H. M. Stationery Office, 1955 [erschienen] 1957
-
3070:
Note on the flow around delta wings with sharp leading edges by G. H. Lee
London: HMSO, 1955 [erschienen] 1958
-
3083:
Experiments on the use of suction through perforated strips for maintaining laminar flow transition and drag measurements by N. Gregory and W. S. Walker
London: H. M. Stationery Office, 1955 [erschienen] 1958
-
3078:
Low speed tunnel model tests on the flow structure behind a delta wing aircraft and a 40 deg swept wing aircraft at high incidences by D. A. Kirby and A. Spence
London: HMSO, 1955 [erschienen] 1958
-
3057:
On the integral equations of two-dimensional subsonic flutter derivative theory by D. E. Williams
London: H. M. Stationery Office, 1955 [erschienen] 1958
-
3065:
The effect of wing tailplane aerodynamic interaction on tail flutter by D. E. Williams
London: H. M. Stationery Office, 1955 [erschienen] 1958
-
3102:
Calculation of the load distribution over a wing with arbitrary camber and twist at sonic speed by K. W. Mangler, and D. G. Randall
London: H. M. Stationery Office, 1955 [erschienen] 1959
-
3067:
Supersonic flow past quasi-cylindrical bodies of almost circular cross section by D. G. Randall
London: H. M. Stationery Office, 1955 [erschienen] 1958
-
3056:
The use of pitot tubes in the measurement of laminar boundary layers in supersonic flow by R. J. Monaghan
London: H. M. Stationery Office, 1955 [erschienen] 1957
-
3085:
The development of slotted working section liners for transonic operation of the R.A.E. Bedford 3-ft Wind Tunnel by E. P. Sutton
London: HMSO, 1955 [erschienen] 1958
-
3079:
The representation of engine airflow in wind tunnel model testing by J. Seddon and L. F. Nicholson
London: HMSO, 1955 [erschienen] 1960
-
3040:
Current tests on laminar boundary layer control by suction through perforations by S. F. J. Butler
London: H. M. Stationery Office, 1957
-
3042:
Experiments at M = 14̓1 on elliptic cones with supersonic leading edges by E. W. E. Rogers and C. J. Berry
London: H. M. Stationery Office, 1955 [erschienen] 1957
-
3045:
Calculated velocity distribution and force derivatives for a series of high-speed aerofoils by C. S. Sinnott
London: H.M. Stationery Office, 1955 [erschienen] 1957
-
3109:
The occurence and development of boundary layer separations at high incidences and high speeds by H. H. Pearcey
London: H. M. Stationery Office, 1955 [erschienen] 1960
-
3208:
Subsonic wind tunnel tests on a crescent winged aircraft, including tests of leading edge droop designs and several tailplane heights by C. N. Hall and B. J. Prior
London: H. M. Stationery Office, 1955 [erschienen] 1961
-
3231:
Flutter tests on some delta wings using ground launched rockets by W. G. Molyneux and F. Ruddlesden
London: HMSO, 1955 [erschienen] 1961
-
3190:
Some observations of the flow over a delta-winged model with 55-deg leading edge sweep, at mach numbers between 0.4 and 1.8 by E. P. Sutton
London: H. M. Stationery Office, 1955 [erschienen] 1960
-
3157:
A method for calculating the lifting forces on wings (unsteady subsonic and supersonic lifting-surface theory) by J. R. Richardson
London: H.M. Stationery Office, 1955 [erschienen] 1960
-
3052:
On the stressing of multi-rib thin wings of low aspect ratio and rectangular plan form by L. S. D. Morley
London: Her Majestys's Stationery Office, 1955 [erschienen] 1958
-
3027:
An investigation of the velocity distribution around the nose of the aerofoil with a flap by Ian H. Rettie
London: H. M. Stationery Office, 1955 [erschienen] 1957
-
3023:
Initial lift of finite aspect ratio wings due to a sudden change of incidence by Doris E. Lehrian
London: H. M. Stationery Office, 1955 [erschienen] 1957
-
3017:
Flight investigation of some airworthiness problems of civil boat seaplanes by J. Taylor, J. E. Allen and A. G. Smith
London: H. M. Stationery Office, 1955 [erschienen] 1958
-
3021:
The effect of the ground on a helicopter rotor in forward flight by I. C. Cheeseman, and W. E. Bennett
London: H. M. Stationery Office, 1955 [erschienen] 1957
-
3025:
Flight experiments on boundary layer control for low drag by M. R. Head, D. Johnson and M. Coxon
London: H. M. Stationery Office, 1955 [erschienen] 1957
-
2946:
Measurement of lift, pitching moment and hinge moment on a two-dimensional cambered aerofoil to assist the estimation of camber derivatives by H. C. Garner; A. S. Batson
London: Her Majesty's Stationery Office, 1955
-
3130:
A new standard for the prediction of full scale spin and recovery characteristics from model tests by T. H. Kerr
London: H. M. Stationery Office, 1955 [erschienen] 1960
-
2994:
Velocities on two-dimensional closed and semi-infinite aerofoils at zero incidence by S. Neumark, and B. Thwaites
London: HMSO, 1955 [erschienen] 1957
-
3001:
Loading conditions of tailed aircraft in longitudinal manoeuvres by T. Czaykowski
London: HMSO, 1956
-
3013:
Internal air-cooling for turbine blades a general design survey by D. G. Ainley
London: HMSO, 1955 [erschienen] 1957
-
3008:
Velocity distribution on thin tapered arrowhead and delta wings with spanwise constant thickness ratio at zero incidence by S. Neumark, J. Collingbourne and E. J. York
London: HMSO, 1955 [erschienen] 1958
-
3011:
The aerodynamic effects of aspect ratio and sweepback on wing flutter by W. G. Molyneux, and H. Hall
London: HMSO, 1955 [erschienen] 1957
-
2979:
The secondary flow in a cascade of turbine blades by W. D. Armstrong
London: HMSO, 1955 [erschienen] 1957
-
3004:
The interaction between shock waves and boundary layers at the trailing edge of a double wedge aerofoil at supersonic speed by B. D. Henshall, and R. F. Cash
London: HMSO, 1955 [erschienen] 1957
-
3005:
Effect of yaw on the compressible laminar boundary layer by J. Tinkler
London: HMSO, 1955 [erschienen] 1957
-
3043:
Tests in the Royal Aircraft Establishment 10 ft x 7 ft high speed tunnel on 50 deg swept back wings by A. B. Haines and C. W. Rhodes
London: H. M. Stationery Office, 1954 [erschienen] 1957
-
3032:
The effects of taper on the supervelocities on three-dimensional wings at zero incidence by K. W. Newby
London: H. M. Stationery Office, 1954 [erschienen] 1957
-
3210:
Elevator flutter involving two tabs by E. G. Broadbent and Mary Clarke
London: H. M. Stationery Office, 1954 [erschienen] 1961
-
2957:
Note on the circulation in circuits which cut the streamlines in the wake of an aerofoil at right angles by J. H. Preston
London: HMSO, 1954 [erschienen] 1956
-
3016:
Measurements of the paths of the vortex cores shed from the wings of a typical guided missile model at M = 15̓7 by R. H. Plascott
London: H. M. Stationery Office, 1954 [erschienen] 1956
-
2965:
The stress distribution in panels bounded by constant stress edge members by E. H. Mansfield
London: HMSO, 1954 [erschienen] 1957
-
3024:
Measurements of the effect of windscreen shapes on the drag of cockpit canopies at transonic and low supersonic speeds using the free flight model technique by C. Kell
London: H. M. Stationery Office, 1954 [erschienen] 1957
-
2953:
The effect of a wind gradient on the rate of climb of an aircraft by W. A. Mair
London: HMSO, 1954 [erschienen] 1957
-
2959:
The torsional rigidity of solid cylinders of double wedge section by E. H. Mansfield
London: HMSO, 1954 [erschienen] 1956
-
2960:
Theoretical load distribution on a wing with vertical plates by J. Weber
London: HMSO, 1954 [erschienen] 1956
-
2916:
Abstracts of papers published externally
London: HMSO, 1954 [erschienen] 1955
-
2988:
An investigation of the high alternating stresses in the blades of an axial flow compressor by J. R. Forshaw
London: HMSO, 1954 [erschienen] 1957
-
3012:
Scale effects at high subsonic and transonic speeds, and methods for fixing boundary layer transition in model experiments by A. B. Haines, D. W. Holder, and H. H. Pearcey
London: HMSO, 1954 [erschienen] 1957
-
2986:
Local coefficients of skin friction and heat transfer for turbulent boundary layers on two-dimensional diffusers by J. N. Hool
London: HMSO, 1954 [erschienen] 1957
-
2993:
The calculation of the pressure distribution on thick wings of small aspect ratio at zero lift in subsonic flow by J. Weber
London: HMSO, 1954 [erschienen] 1957
-
2977:
The reflection effect of fences at low speeds by J. Weber, and J. A. Lawford
London: HMSO, 1954 [erschienen] 1956
-
2989:
A survey of the alternating pressures exciting high frequency vibrations in gas turbines by J. R. Forshaw
London: HMSO, 1954 [erschienen] 1956
-
2992:
Theoretical loan distributions on fin body tailplane arrangements in a sine wind by J. Weber, and A. C. Hawk
London: HMSO, 1954 [erschienen] 1957
-
2991:
One-dimensional treatment of non-uniform flow by R. D. Tyler
London: HMSO, 1954 [erschienen] 1957
-
2998:
An empirical analysis of the planing lift characteristics of rectangular flat plates and wedges by P. Ward Brown
London: HMSO, 1954 [erschienen] 1957
-
3003:
The strength of annealed and heat treated glass by F. G. J. Brown, and J. Ellis
London: HMSO, 1954 [erschienen] 1957
-
3014:
Flight tests on a Vampire Mk. 5 with a redesigned anti-snaking rudder by W. J. G. Pinsker
London: HMSO, 1954 [erschienen] 1957
-
3192:
Some notes on the flow patterns observed over various swept-back wings at low Mach numbers (in the R.A.E. 10-ft x 7-ft high speed tunnel) by A. B. Haines
London: H. M. Stationery Office, 1954 [erschienen] 1960
-
3049:
Theory of aerofoils on which occur bubbles of stationary air by L. C. Woods
London: H. M. Stationery Office, 1953 [erschienen] 1957
-
3096:
An analysis of steady straight flight with inclined thrust by S. B. Gates and A. W. Thorpe
London: H. M. Stationery Office, 1953 [erschienen] 1959
-
3101:
The R. A. E. electronic simulator for flutter investigations in six degrees of freedom or less by F. Smith and W. D. T. Hicks
London: H. M. Stationery Office, 1953 [erschienen] 1959
-
3033:
A survey and correlation of data on heat transfer by forced convection at supersonic speeds by R. J. Monaghan
London: H. M. Stationery Office, 1953 [erschienen] 1958
-
3141:
Wind tunnel tests on the effect of a localised mass on the flutter of a swept back wing with fixed root by D. R. Gaukroger
London: H. M. Stationery Office, 1953 [erschienen] 1960
-
3165:
Balance and pressure measurements at high subsonic speeds on a model of a swept wing aircraft (Hawker P.1052) and some comparisons with flight data by J. R. Collingbourne and A. C. S. Pindar
London: Her Majesty's Stationery Office, 1953 [erschienen] 1960
-
3035:
The estimation of shock pressure recovery and external drag of conical centre body intakes at supersonic speeds by E. L. Goldsmith and C. F. Griggs
London: H. M. Stationery Office, 1953 [erschienen] 1959
-
3188:
Aileron control of small-aspect-ratio aircraft in particular, delta aircraft by W. J. G. Pinsker
London: H. M. Stationery Office, 1953 [erschienen] 1960
-
2962:
Control surfaces restrained by viscous friction as a means of damping aircraft oscillations by W. J. G. Pinsker
London: HMSO, 1953 [erschienen] 1957
-
2938:
An experimental investigation of the effects of deformation on the aerodynamic characteristics of a swept back wing by Joseph Black
London: HMSO, 1953 [erschienen] 1956
-
2966:
Calculations of the pressure distributions and boundary layer development on a body of revolution with various parabolic afterbodies at supersonic speeds by L. E. Fraenkel
London: HMSO, 1953 [erschienen] 1957
-
2945:
The time vector method for stability investigations by K. H. Doetsch
London: HMSO, 1953 [erschienen] 1957
-
2947:
The calculation of the loading and pressure distribution on cranked wings by G. G. Brebner
London: HMSO, 1953 [erschienen] 1955
-
2937:
The forward take-off of a helicopter by F. O'Hara
London: HMSO, 1953 [erschienen] 1957
-
2948:
Interference corrections for asymmetrically loaded wings in closed rectangular wind tunnels by H. C. Garner and W. E. A. Acum
London: HMSO, 1953 [erschienen] 1957
-
2932:
Aerodynamic flutter coefficients for subsonic, sonic and supersonic flow (linear two-dimensional theory) by P. F. Jordan
London: HMSO, 1953 [erschienen] 1957
-
2933:
Flow instability of centre body diffusers at supersonic speeds by D. Beastall
London: HMSO, 1953 [erschienen] 1956
-
2949:
Some flutter tests on swept back wings using ground launched rockets by W. G. Molyneux and F. Ruddlesden
London: HMSO, 1953 [erschienen] 1956
-
3038:
The harmonically oscillating wing with finite vortex trail by P. F. Jordan
London: Her Majestys's Stationery Office, 1953 [erschienen] 1957
-
2833:
An unconventional type of fatigue testing machine by F. Aughtie, and H. L. Cox
London: HMSO, 1953 [erschienen] 1955
-
2987:
The component pressure losses in combustion chambers by H. A. Knight and R. B. Walker
London: HMSO, 1953 [erschienen] 1957
-
2983:
Problems of longitudinal stability below minimum drag speed, and theory of stability under constraint by S. Neumark
London: HMSO, 1953 [erschienen] 1957
-
2911:
Wind tunnel tests on the symmetric and antisymmetric flutter of swept-back wings by D. R. Gaukroger
London: HMSO, 1953 [erschienen] 1955
-
2922:
Calculation of stability derivatives for oscillating wings by Doris E. Lehrian
London: HMSO, 1956
-
2923:
Hinge moment derivatives for an oscillating control by C. S. Sinnott
London: HMSO, 1953 [erschienen] 1955
-
2985:
The design and testing of an axial compressor having a mean stage temperature rise of 30 deg C by A. D. S. Carter, S. J. Andrews and E. A. Fielder
London: HMSO, 1953 [erschienen] 1957
-
2927:
Tests on a single stage turbine comparing the performance of twisted with untwisted rotor blades by I. H. Johnston and L. R. Knight
London: HMSO, 1953 [erschienen] 1956
-
2918:
The calculation of the pressure distribution over the surface of two-dimensional and swept wings with symmetrical aerofoil sections by J. Weber
London: HMSO, 1953 [erschienen] 1955
-
2972:
Preliminary report on a gust alleviator investigation on a Lancaster aircraft by J. Zbrozek, K. W. Smith and D. White
London: HMSO, 1953 [erschienen] 1957
-
2921:
The oscillating aerofoil in subsonic flow by W. P. Jones
London: HMSO, 1953 [erschienen] 1956
-
2969:
Theory of aerofoil spoilers by L. C. Woods
London: HMSO, 1953 [erschienen] 1956
-
2971:
The buckling shear stress of simply supported, infinitely long plates with transverse stiffeners by P. W. Kleeman
London: Her Majesty's Stationery Office, 1953 [erschienen] 1956
-
2978:
Wind-tunnel flutter tests on a delta wing with an all-moving tip control surface by D. R. Gaukroger
London: HMSO, 1953 [erschienen] 1956
-
3084:
The R.A.E. Hollerith punched card installation (1945 - 1952) by R. A. Fairthorne, G. J. Griffith and M. F. C. Woollett
London: HM Stationery Office, 1952 [erschienen] 1958
-
3030:
Some actuator disc theories for the flow of air trough an axial turbo machine by J. H. Horlock
London: H. M. Stationery Office, 1952 [erschienen] 1958
-
3073:
On the post buckling behaviour of stiffened plane sheet under shear by E. H. Mansfield
London: H. M. Stationery Office, 1952 [erschienen] 1958
-
2940:
Analysis of short period longitudinal oscillations of an aircraft - interpretation of flight tests by S. Neumark
London: HMSO, 1952 [erschienen] 1956
-
2951:
Tests in the R.A.E. 10 ft x 7 ft High Speed Wind Tunnel on drop tanks fitted to two swept back wings
London: HMSO, 1952 [erschienen] 1956
-
2963:
V-g records from Vampire aircraft (March 1951 - October 1951) by E. Marjorie Owen and J. R. Heath-Smith
London: HMSO, 1952 [erschienen] 1956
-
3151:
The effect of diameter ratio on the performance of a low stagger axial compressor stage by R. A. Jeffs and R. G. Adams
London: H. M. Stationery Office, 1952 [erschienen] 1960
-
2898:
The full-scale hydrodynamic performance of a large four-engined flying boat at overload in calm water and swell by J. A. Hamilton and R. V. Gigg
London: HMSO, 1952 [erschienen] 1956
-
2997:
Second harmonic control on the helicopter rotor by W. Stewart
London: HMSO, 1952 [erschienen] 1957
-
2885:
Multhopp's subsonic lifting surface theory of wings in slow pitching oscillations by H. C. Garner
London: HMSO, 1952 [erschienen] 1956
-
3007:
The effect of a spike protruding in front of a bluff body at supersonic speeds by D. Beastall and J. Turner
London: Her Majesty's Stationery Office, 1952 [erschienen] 1957
-
2919:
Effects of Reynolds number on the flow of air through a cascade of compressor blades by H. G. Rhoden
London: HMSO, 1952 [erschienen] 1956
-
2899:
A full-scale investigation into the hydrodynamic behaviour of a highly faired flying boat hull by J. A. Hamilton
London: HMSO, 1952 [erschienen] 1956
-
2999:
R.A.E. high-speed wind-tunnel tests of the trailing edge controls on a delta wing with 52 deg sweepback by K. W. Newby
London: HMSO, 1952 [erschienen] 1957
-
2924:
A method of calculating the short period longitudinal stability derivatives of a wing in linearised unsteady compressible flow by K. W. Mangler
London: HMSO, 1952 [erschienen] 1957
-
2886:
Pressure and boundary-layer measurements on a two-dimensional wing at low speed by G. G. Brebner; J. A. Bagley
London: Her Majesty's Stationery Office, 1952 [erschienen] 1956
-
2499:
Transition and drag measurements on the Boulton Paul sample of laminar flow wing construction
London: HMSO, 1952
-
2845:
Aerofoil design in two-dimensional subsonic compressible flow by L. C. Woods
London: HMSO, 1952 [erschienen] 1955
-
2926:
Some remarks on Multhopp's subsonic lifting surface theory by K. W. Mangler and B. F. R. Spencer
London: HMSO, 1952 [erschienen] 1956
-
2920:
Analysis of Reynolds number effects in fluid flow through two-dimensional cascades by D. J. K. Stuart
London: HMSO, 1952 [erschienen] 1955
-
2984:
The flow at the mouth of a Stanton Pitot by A. Thom
London: HMSO, 1952 [erschienen] 1956
-
2995:
Low speed wind-tunnel tests on two thin cranked wings with 60 deg sweepback inboard by C. J. Mansell
London: HMSO, 1952 [erschienen] 1957
-
2996:
Low speed tunnel tests of some split flap arrangements on a 48 deg delta wing parts 1 and 2
London: HMSO, 1952 [erschienen] 1957
-
2873:
The effect of tight clamping on the fatigue strength of joints by W. A. P. Fisher and W. J. Winkworth
London: HMSO, 1952 [erschienen] 1955
-
3009:
Low speed wind-tunnel measurements of longitudinal oscillatory derivatives on three wing plan forms by G. F. Moss
London: HMSO, 1952 [erschienen] 1957
-
3110:
Air cooling methods for gas turbine combustion systems by F. J. Bayley
London: H. M. Stationery Office, 1951 [erschienen] 1959
-
3112:
A frost point hygrometer for supersonic wind tunnels (with addendum) by D. Beastall and A. Winyard
London: H. M. Stationery Office, 1951 [erschienen] 1959
-
3127:
An assessment of the probable causes of variation of the speed correction coefficient of aircraft thermometers by D. D. Clark
London: H. M. Stationery Office, 1951 [erschienen] 1959
-
3117:
Helicopter behaviour in the vortex ring conditions by W. Stewart
London: H. M. Stationery Office, 1951 [erschienen] 1959
-
2964:
The influence of rope stretch on tension variations in arresting gears by N. I. Bullen
London: HMSO, 1951 [erschienen] 1956
-
2955:
Experiments with slotted and perforated walls in a two-dimensional high speed tunnel by D. W. Holder, R. J. North and A. Chinneck
London: HMSO, 1951 [erschienen] 1956
-
2944:
Technique for flutter tests using ground launched rockets, with results for unswept wings by W. G. Molyneux, F. Ruddlesden and P. J. Cutt
London: HMSO, 1951 [erschienen] 1956
-
2910:
Model tests on the asymmetry of airflow occuring in twin-intake systems at subsonic speeds by J. Seddon and W. J. G. Trebble
London: HMSO, 1951 [erschienen] 1955
-
2841:
Aerodynamic coefficients for an oscillating delta wing by Doris E. Lehrian
London: HMSO, 1951 [erschienen] 1957
-
2867:
The theory of torsional vibrations of a four-boom thin walled cylinder of rectangular cross-section by E. H. Mansfield
London: HMSO, 1951 [erschienen] 1955
-
2888:
Calculation of the pressure distribution over a wing at sonic speeds by K. W. Mangler
London: HMSO, 1951 [erschienen] 1955
-
2809:
Control effectiveness tests at transonic speeds on an EC.1250 section with 0.25 chord concave control by T. Lawrence
London: HMSO, 1951 [erschienen] 1955
-
2848:
The geared elevator tab and tail unit stiffness requirements by Ll. T. Niblett
London: HMSO, 1951 [erschienen] 1955
-
2881:
Control testing in wind tunnels by L. W. Bryant, and H. C. Garner
London: HMSO, 1951 [erschienen] 1956
-
2974:
A method of performance estimation for axial flow turbines by D. G. Ainley and G. C. R. Mathieson
London: Her Majesty's Stationery Office, 1951 [erschienen] 1957
-
2890:
The reduction to standard conditions of take-off measurements on turbo-jet aircraft by G. Jackson. With an app. by K. J. Lush
London: HMSO, 1951 [erschienen] 1957
-
2846:
Alternating pressures and blade stresses in an axial flow compressor by J. R. Forshaw, H. Taylor, and R. Chaplin
London: HMSO, 1951 [erschienen] 1956
-
2929:
Tests concerning novel designs of blades for axial compressors by S. J. Andrews, R. A. Jeffs and E. L. Hartley
London: HMSO, 1951 [erschienen] 1956
-
3000:
An analysis of available data on the local aerodynamic centres of aerofoils in two- and three-dimensional flow by A. S. Taylor
London: HMSO, 1951 [erschienen] 1957
-
2905:
The RAE 4 ft x 3 ft experimental low turbulence wind tunnel 2 Measurements of turbulence intensity and noise in the working-section / by H. Schuh and K. G. Winter
London: HMSO, 1951 [erschienen] 1957
-
2907:
An approximation to the slow mode of longitudinally disturbed motion of an aircraft in level flight by A. W. Thorpe
London: HMSO, 1951 [erschienen] 1957
-
2861:
Helicopter rotor behaviour after engine failure in forward flight by W. Stewart, and M. F. Burle
London: HMSO, 1951 [erschienen] 1955
-
2863:
Tests at high subsonic speeds on a 10 per cent thick pressure plotting aerofoil of RAE 104 section by E. W. E. Rogers, C. J. Berry, and R. F. Cash
London: HMSO, 1951 [erschienen] 1956
-
2864:
Force and moment measurements on a conical body and a rectangular wing, separately and in combination, at Mach number 19̓4 by J. R. Anderson and D. Treadgold
London: HMSO, 1951 [erschienen] 1956
-
2887:
The aerodynamic derivatives with respect to a rate of yaw for a delta wing with dihedral and at incidence at supersonic speeds by J. H. Hunter-Tod
London: HMSO, 1951 [erschienen] 1957
-
2779:
The effect on transition of isolated surface excrescences in the boundary layer by N. Gregory, and W. S. Walker
London: HMSO, 1951 [erschienen] 1956
-
2851:
Tunnel wall effect on an aerofoil at subsonic speeds by A. Thom and Laura Klanfer
London: HMSO, 1951 [erschienen] 1957
-
2865:
Some applications of the Lamé function solutions of the linearised supersonic flow equations by G. M. Roper
London: HMSO, 1951 [erschienen] 1955
-
2870:
A simplified treatment of a fixed root swept wing built on Hill's isoclinic principle by D. Williams
London: HMSO, 1951 [erschienen] 1956
-
2973:
Estimation of the change in performance characteristics of a turbine resulting from changes in the gas thermodynamic properties by D. G. Ainley
London: HMSO, 1951 [erschienen] 1956
-
2564:
Measurement of aircraft attitude relative to flight path during dives by J. E. H Braybon
London: H.M.S.O., 1951
-
3062:
An experimental investigation of the effect of engine loads on wing structures by J. L. Reddaway
London: H. M. Stationery Office, 1950 [erschienen] 1957
-
3019:
An approximate method of estimating the effect of elastic deformability of the aircraft structure on the manoeuvre point parts 1 and 2 by H. Fingado, and A. S. Taylor
London: H. M. Stationery Office, 1950 [erschienen] 1957
-
2883:
An experimental investigation of a thick aerofoil nozzle cascade by S. J. Andrews and N. W. Schofield
London: HMSO, 1950 [erschienen] 1956
-
2981:
Measurement and suppression of tension waves in arresting gear rope systems by J. M. N. Willis, S. W. Chisman and N. I. Bullen
London: HMSO, 1950 [erschienen] 1957
-
2826:
Wind tunnel flutter tests on a model delta wing under fixed and free root conditions by D. R. Gaukroger, E. W. Chapple, and A. Milln
London: HMSO, 1950 [erschienen] 1955
-
2893:
A wind tunnel technique for flutter investigations on swept wings with body freedoms by P. F. Jordan and F. Smith
London: HMSO, 1950 [erschienen] 1955
-
3015:
Enthalpy charts: for dissociating gas mixtures in the temperature range 600 deg to 4000 deg K by H. Reichert
London: HMSO, 1950 [erschienen] 1957
-
2375:
Flight tests on "King Cobra" FZ. 440 to investigate the practical requirements for the achievement of low profile drag coefficients on a "low drag" aerofoil by F. Smith; D. J. Higton
London: His Majesty's Stationery Office, 1950
-
2795:
Theoretical supersonic drag of non-lifting infinite span wings swept behind the Mach lines by T. Nonweiler
London: HMSO, 1950 [erschienen] 1954
-
2869:
The flutter properties of a simple aero-isoclinic wing system by N. C. Lambourne and A. Chinneck
London: HMSO, 1950 [erschienen] 1956
-
2828:
Flutter problems of high-speed aircraft by E. G. Broadbent
London: HMSO, 1949 [erschienen] 1955
-
2476:
The effect of the sweepback of delta wings on the performance of an aircraft at supersonic speeds by A. Robinson, and F. T. Davies
London: HMSO, 1947 [erschienen] 1951
-
2843:
Low speed wind tunnel tests on a model of a jet tailless aircraft by J. Trouncer, and G. F. Moss
London: HMSO, 1947 [erschienen] 1956
-
2818:
Swept wings in supersonic flight by S. B. Gates
London: HMSO, 1946 [erschienen] 1954
-
2078:
The disturbed longitudinal motion of an uncontrolled aircraft and of an aircraft with automatic control by S. Neumark
London: HMSO, 1943 ersch. 1947
-
3250:
Published reports and memoranda of the Aeronautical Research Council
[London]: [HMSO], 1936
-
3303:
The design of Michell optimum structures by A. S. L. Chan
London: H. M. Stationery Office, 1069 [erschienen] 1962