> Details
Alksne, Alberta Y.
[Other];
Allen, H. Julian
[Other];
Anderson, Seth B.
[Other];
Barnett, Henry C.
[Other];
Beckwith, Ivan E.
[Other];
Belles, Frank E.
[Other];
Blackshear, Perry L.
[Other];
Boatright, William B.
[Other];
Breitwieser, Roland
[Other];
Brooks, George W.
[Other];
Brown, B. Porter
[Other];
Cahen, George L.
[Other];
Cahn, Maurice S.
[Other];
Callaghan, Edmund E.
[Other];
Chapman, Dean R.
[Other];
Coleman, Robert P.
[Other];
Coles, Willard D.
[Other];
Cook, William P.
[Other];
Cook, Woodrow L.
[Other];
Freeman. J.W
[Other];
Felix, A. Richard
[Other];
Von Doenhoff, Albert E.
[Other];
Evans, Albert J.
[Other];
Pearson, Albin O.
[Other];
[...]
;
United States Congress Senate,
United States President (1953-1961 : Eisenhower),
United States National Advisory Committee for Aeronautics,
California Institute of Technology,
Stanford University,
University of Michigan
Forty-fourth annual report of the National Advisory Committee for Aeronautics, 1958. Administrative report including technical reports Nos. 1342 to 1392. (Final report)
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- Media type: E-Book
- Title: Forty-fourth annual report of the National Advisory Committee for Aeronautics, 1958. Administrative report including technical reports Nos. 1342 to 1392. (Final report)
- Contributor: Alksne, Alberta Y. [Other]; Allen, H. Julian [Other]; Anderson, Seth B. [Other]; Barnett, Henry C. [Other]; Beckwith, Ivan E. [Other]; Belles, Frank E. [Other]; Blackshear, Perry L. [Other]; Boatright, William B. [Other]; Breitwieser, Roland [Other]; Brooks, George W. [Other]; Brown, B. Porter [Other]; Cahen, George L. [Other]; Cahn, Maurice S. [Other]; Callaghan, Edmund E. [Other]; Chapman, Dean R. [Other]; Coleman, Robert P. [Other]; Coles, Willard D. [Other]; Cook, William P. [Other]; Cook, Woodrow L. [Other]; Freeman. J.W [Other]; Felix, A. Richard [Other]; Von Doenhoff, Albert E. [Other]; Evans, Albert J. [Other]; Pearson, Albin O. [Other]; Feingold, Arnold M. [Other]; Curren, Arthur N. [Other]; Vogeley, Arthur W. [Other]; Gammon, Benson E. [Other]; Shufflebarger, C.C. [Other]; Taylor, C.F. [Other]; Wilts, C.H. [Other]; Graves, Charles C. [Other]; May, Charles E. [Other]; Shuford, Charles L. [Other]; Payne, Chester B. [Other]; Kuehn, Donald M. [Other]; Eisenhower, Dwight D. [Other]; Jonash, Edmund R. [Other]; Hoffman, Edward L. [Other]; Perkins, Edward W. [Other]; Stowell, Elbridge Z. [Other]; Reshotku, Eli [Other]; Horton, Elmer A. [Other]; Schum, Eugene F. [Other]; Gustafson, F.B. [Other]; Schlechte, Floyd R. [Other]; Diederich, Franklin W. [Other]; Fuller, Franklyn B. [Other]; Preston, G. Merritt [Other]; Liner, George [Other]; Cooper, George E. [Other]; Pesman, Gerard J. [Other]; Lindberg, H.E. [Other]; Larson, Howard K. [Other]; Flugge-Lotz, I. [Other]; Pinkel, I. Irving [Other]; Drell, Isadore L. [Other]; Esgar, Jack B. [Other]; Grobman, Jack S. [Other]; Emery, James C. [Other]; Wear, Jerrold D. [Other]; Houbolt, John C. [Other]; Rowe, John P. [Other]; Erwin, John R. [Other]; Spreiter, John R. [Other]; Herrig, L. Joseph [Other]; Jorgensen, Leland H. [Other]; Sternfield, Leonard [Other]; Tower, Leonard K. [Other]; Lassiter, Leslie W. [Other]; Fisher, Lewis R. [Other]; Fisher, Lloyd J. [Other]; Vosteen, Louis F. [Other]; Pinns, M.L. [Other]; Kelly, Mark W. [Other]; Heaslet, Max A. [Other]; Kurbjun, Max C. [Other]; Van Dyke, Milton D. [Other]; Hill, P.R. [Other]; Decker, R.F. [Other]; Wright, Ray H. [Other]; Heldenfels, Richard R. [Other]; Innis, Robert C. [Other]; Tapscott, Robert J. [Other]; Hess, Robert W. [Other]; Sommer, Simon C. [Other]; Weiss, Solomon [Other]; Neice, Stanford E. [Other]; Rossow, Vernon J. [Other]; Ritchie, Virgil S. [Other]; Olson, W.T. [Other]; Gracey, William [Other]; Eggers, Alfred J. [Other]; McComb, Harvey G. [Other]; Sanders, J. Lyell [Other]
- Corporation: United States, President (1953-1961 : Eisenhower) ; United States, National Advisory Committee for Aeronautics ; California Institute of Technology ; Stanford University ; University of Michigan
-
imprint:
Washington, DC, 1959
Online-Ausg.: Chester, Vt: NewsBank, inc, 2008 -
Published in:
United States congressional serial set ; serial set no. 12180
Senate document / 86th Congress, 1st session. Senate ; no. 6 - Extent: Online-Ressource (1503 p); illustrations, tables
- Language: English
- Reproductino series: U.S. Congressional Serial Set, 1817-1980
- Type of reproduction: Online-Ausg.
- Place of reproduction: Chester, Vt: NewsBank, inc, 2008
- Origination:
-
Footnote:
A comparative analysis of the performance of long-range hypervelocity vehicles, by Alfred J. Eggers, Jr., H. Julian Allen, and Stanford E. Neice, NACA [No. 1382], p. 1141
A correlation of results of a flight investigation with results of an analytical study of effects of wing flexibility on wing strains due to gusts, by C.C. Shufflebarger, Chester B. Payne, and George L. Cahen, NACA [No. 1365], p. 669
A low-speed experimental investigation of the effect of a sandpaper type of roughness on boundary layer transition, by Albert F. Von Doenhoff and Elmer A. Horton, NACA [No. 1349], p. 239
A method for simulating the atmospheric entry of long-range ballistic missiles, by A.J. Eggers, Jr., NACA [No. 1378], p. 1009
A method of computing the transient temperature of thick walls form arbitrary variation of adiabatic-wall temperature and heat-transfer coefficient, by P.R. Hill, NACA [No. 1372], p. 877
A phenomenological relation between stress, strain rate, and temperature for metals at elevated temperatures, by Elbridge Z. Stowell, NACA [No. 1343], p. 125
A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver, by Leonard Sternfield, NACA [No. 1344], p. 131
A study of the motion and aerodynamic heating of ballistic missiles entering the earth's atmosphere at hight supersonic speeds, by H. Julian Allen and A.J. Eggers, Jr. NACA [No. 1381], p. 1125
A summary of preliminary investigations into the characteristics of combustion screech in ducted burners, by Lewis Laboratory Staff, NACA [No. 1384], p. 1195
A theoretical and experimental study of planing surfaces including effects of cross section and plan form, by Charles L. Shuford, Jr., NACA [No. 1355], p. 373
A variational theorem for creep with applications to plates and columns, by J. Lyell Sanders, Jr., Harvey G. McComb, Jr., and Floyd R. Schlechte, NACA [No. 1342], p. 117
A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96, by Albert J. Evans and George Liner, NACA [No. 1375], p. 933
An analysis of pressure studies and experimental and theoretical downwash and sidewash behind five pointed-tip wings at supersonic speeds, by William B. Boatright, NACA [No. 1380], p. 1067
An experimental investigation of sting-support effects on drag and a comparison with jet effects at transonic speeds, by Maurice S. Cahn, NACA [No. 1353], p. 327
Approximate analysis of effects of large deflections and initial twist on torsional stiffness of a cantilever plate subjected to thermal stresses, by Richard R. Heldenfels and Louis F. Vosteen, NACA [No. 1361], p. 593
Area-suction boundary-layer control as applied to the trailing-edge flaps of a 35 [degree] swept-wing airplane, by Woodrow L. Cook, Seth B. Anderson, and George E. Cooper, NACA [No. 1370], p. 823
Blowing-type boundary-layer control as applied to the trailing-edge flaps of a 25 [degree] swept-wing airplane, by Mark W. Kelly, Seth B. Anderson, and Robert C. Innis, NACA [No. 1369], p. 799
Boron and zirconium from crucible refractories in a complex heat-resistant alloy, by R.F. Decker, John P. Rowe, and J.W. Freeman, University of Michigan, [No. 1392], p. 1457
Calculated and measured stresses in simple panels subject to intense random acoustic loading including the near noise field of a turbojet engine, by Leslie W. Lassiter and Robert W. Hess, NACA [No. 1367], p. 703
Characteristics of the Langley 8-foot transonic tunnel with slotted test section, by Ray H. Wright, Virgil S. Ritchie, and Albin O. Pearson, NACA [No. 1389], p. 1297
Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number, by Eli Reshotku and Ivan E. Beckwith, NACA [No. 1379], p. 1016
Differential equations of motion for combined flapwise vending, chordwise bending, and torsion of twisted non-uniform rotor blades, by John C. Houbolt and George W. Brooks, NACA [No. 1346], p. 179
Ditching investigations of dynamic models and effects of design parameters on ditching characteristics, by Lloyd J. Fisher and Edward L. Hoffman, NACA [No. 1347], p. 197
Drag minimization for wings and bodies in supersonic flow, by Max A. Heaslet and Franklyn B. Fuller, NACA [No. 1385], p. 1213
Effect of chord size on weight and cooling characteristics of air-cooled turbine blades, by Jack B. Esgar, Eugene F. Schum, and Arthur N. Curren, NACA [No. 1354], p. 359
Effect of fuel variables on carbon formation in turbojet-engine combustors, by Edmund R. Jonash, Jerrold D. Wear, and William P. Cook, NACA [No. 1352], p. 309
Elliptic cones alone and with wings at supersonic speeds, by Leland H. Jorgensen, NACA [No. 1376], p. 975
Experimental determination of effects of frequency and amplitude on the lateral stability derivatives for a delta, a swept, and an unswept wing oscillating in yaw, by Lewis R. Fisher, NACA [No. 1357], p. 461
Full-scale investigation of several jet-engine noise-reduction nozzles, by Willard D. Coles and Edmund E. Callaghan, NACA [No. 1387], p. 1249
Ground simulator studies of the effects of valve friction, stick friction, flexibility, and backlash on power control system quality, by B. Porter Brown, NACA [No. 1348], p. 225
Growth of disturbances in a flame-generated shear region, by Perry L. Blackshear, Jr., NACA [No. 1360], p. 546
Incompressible flutter characteristics of representative aircraft wings, by C.H. Wilts, California Institute of Technology, [No. 1390], p. 1385
Investigation of a nonlinear control system, by I. Flugge-Lotz, C.F. Taylor, and H.E. Lindberg, Stanford University, [No. 1391], p. 1423
Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition, by Dean R. Chapman, Donald M. Kuehn, and Howard K. Larson, NACA [No. 1356], p. 419
Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 2, by Leland H. Jorgensen and Edward W. Perkins, NACA [No. 1371], p. 857
Investigation of the drag of various axially symmetric nose shapes of fineness ratio 3 for Mach numbers from 1.24 to 7.4, by Edward W. Perkins, Leland H. Jorgensen, and Simon C. Sommer, NACA [No. 1386], p. 1231
List of technical reports, p. III
Measurement of static pressure on aircraft, by William Gracey, NACA [No. 1364], p. 643
Measurements of free-space oscillating pressures near propellers at flight Mach numbers to 0.72, by Max C. Kurbjun and Arthur W. Vogeley, NACA [No. 1377], p. 999
Methods for obtaining desired helicopter stability characteristics and procedures for stability predictions, by F.B. Gustafson and Robert J. Topscott, NACA [No. 1350], p. 255
NACA Research on slurry fuels, by M.L. Pinns, W.T. Olson, H.C. Barnett, and R. Breitwieser, NACA [No. 1388], p. 1273
On flow of electrically conducting fluids over a flat plate in presence of a transverse magnetic field, by Vernon J. Rossow, NACA [No. 1358], p. 489
Origin and prevention of crash fires in turbojet aircraft, by I. Irving Pinkel, Solomon Weiss, G. Merritt Preston, and Gerard J. Pesman, NACA [No. 1363], p. 623
Survey of hydrogen combustion properties, by Isadore L. Drell and Frank E. Belles, NACA [No. 1383], p. 1161
Systemic two-dimensional cascade tests of NACA 65-Series compressor blades at low speeds, by James C. Emery, L. Joseph Herrig, John R. Erwin, and A. Richard Felix, NACA [No. 1368], p. 713
Table of contents, p. II
The mechanism of thermal-gradient mass transfer in the sodium hydroxide - nickel system, by Charles E. May, NACA [No. 1366], p. 683
The response of an airplane to random atmospheric disturbances, by Franklin W. Diederich, NACA [No. 1345], p. 142
The similarity rules for second-order subsonic and supersonic flow, by Milton D. Van Dyke, NACA [No. 1374], p. 925
Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus- and liner cross-sectional areas, by Charles C. Graves and Jack S. Grobman, NACA [No. 1373], p. 899
Theoretical combustion performance of several high-energy fuels for ramjet engines, by Leonard K. Tower, Roland Breitwieser, and Benson E. Gammon, NACA [No. 1362], p. 605
Theory of self-excited mechanical oscillations of helicopter rotors with hinged blades, by Robert P. Coleman and Arnold M. Feingold, NACA [No. 1351], p. 267
Thin airfoil theory based on approximate solution of the transonic flow equation, by John R. Spreiter and Alberta Y. Alksne, NACA [No. 1359], p. 509
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