Aeronautics. Seventeenth annual report of the National Advisory Committee for Aeronautics. 1931. Including Technical Reports Nos. 365 to 400

Medientyp: E-Book

Titel: Aeronautics. Seventeenth annual report of the National Advisory Committee for Aeronautics. 1931. Including Technical Reports Nos. 365 to 400

Körperschaft: United States, National Advisory Committee for Aeronautics

Erschienen: Washington, DC, 1932
Online-Ausg., Chester, Vt: NewsBank, inc, 2007

Umfang: Online-Ressource (730 p); illustrations, maps, tables

Sprache: Englisch

Reproduktionsreihe: U.S. Congressional Serial Set, 1817-1980

Art der Reproduktion: Online-Ausg.

Hersteller der Reproduktion: Chester, Vt: NewsBank, inc, 2007

Entstehung:

Anmerkungen: A method of flight measurement of spins, by Hartley A. Soule and Nathan F. Scudder [No. 377], p. 267
A new chart for estimating the absolute ceiling of an airplane, by Walter S. Diehl [No. 368], p. 111
A new principle of sound frequency analysis, by Theodore Theodorsen [No. 395], p. 605
Aerodynamic characteristics of circular-arc airfoils at high speeds, by L.J. Briggs and H.L. Dryden [No. 365], p. 67
Airship model tests in the variable density wind tunnel, by Ira H. Abbott [No. 394], p. 583
Coefficients of discharge of fuel injection nozzles for compression-ignition engines, by A.G. Gelalles [ No. 373], p. 193
Comparison of full-scale propellers having R.A.F.-6 and Clark Y airfoil sections, by Hugh B. Freeman [No. 378], p. 283
Dynamic and flight tests on rubber-cord and oleo-rubber-disk landing gears for an F6C-4 airplane, by William C. Peck [No. 366], p. 79
Effect of variation of chord and span of ailerons on hinge moments at several angles of pitch, by B.H. Monish [No. 370], p. 137
Elastic instability of members having sections common in aircraft construction, by George W. Trayer and H.W. March [No. 382], p. 373
Flame movement and pressure development in an engine cylinder, by Charles F. Marvin, Jr., and Robert D. Best [No. 399], p. 697
Full-scale tests of metal propellers at high tip speeds, by Donald H. Wood [No. 375], p. 237
Hydraulics of fuel injection pumps for compression-ignition engines, by A.M. Rothrock [No. 396], p. 621
Investigation of damping liquids for aircraft instruments -- II, by M.R. Houseman and G.H. Keulegan [No. 398], p. 679
Investigation of the diaphragm-type pressure cell, by Theodore Theodorsen [No. 388], p. 507
Maneuverability investigation of an F6C-4 fighting airplane, by C.H. Dearborn and H.W. Kirschbaum [No. 386], p. 475
Maneuverability investigation of the F6C-3 airplane with special flight instruments, by C.H. Dearborn and H.W. Kirschbaum [No. 369], p. 117
On the theory of wing sections with particular reference to the lift distribution, by Theodore Theodorsen [No. 383], p. 411
Present status of aircraft instruments, by Subcommittee on Instruments [No. 371], p. 153
Pressure distribution over a thick, tapered and twisted monoplane wing model -- N.A.C.A. 81 J, by Carl J. Wenzinger [No. 367], p. 97
Pressure distribution over the fuselage of a PW-9 pursuit airplane in flight, by Richard V. Rhode and Eugene E. Lundquist [No. 380], p. 327
Reduction of turbulence in wind tunnels, by Hugh L. Dryden [No. 392], p. 557
Rolling moments due to rolling and yaw for four wing models in rotation, by Montgomery Knight and Carl J. Wenzinger [No. 379], p. 301
Some approximate equations for the standard atmosphere, by Walter S. Diehl [No. 376], p. 257
Span-load distribution as a factor in stability in roll, by Montgomery Knight and Richard W. Noyes [No. 393], p. 567
Static, drop, and flight tests on Musselman type airwheels, by William C. Peck and Albert P. Beard [No. 381], p. 355
Table of contents, p. VI
The aerodynamic characteristics of a slotted Clark Y wing as affected by the auxiliary airfoil position, by Carl J. Wenzinger and Joseph A. Shortal [No. 400], p. 707
The aerodynamic characteristics of eight very thick airfoils from tests in the variable density wind tunnel, by Eastman N. Jacobs [No. 391], p. 545
The automotive ignition coil, by T.H. Darnell [No. 374], p. 211
The comparative performance of superchargers, by Oscar W. Schey [No. 384], p. 425
The drag characteristics of several airships determined by deceleration tests, by F.J. Thompson and H.W. Kirschbaum [No. 397], p. 665
The effect of small angles of yaw and pitch on the characteristics of airplane propellers, by Hugh B. Freeman [No. 389], p. 523
The effect of valve timing upon the performance of a supercharged engine at altitude and an unsupercharged engine at sea level, by Oscar W. Schey and Arnold E. Biermann [No. 390], p. 533
The gaseous explosive reaction -- the effect of pressure on the rate of propagation of the reaction zone and upon the rate of molecular transformation, by F.W. Stevens [No. 372], p. 175
The vertical wind tunnel of the National Advisory Committee for Aeronautics, by Carl J. Wenzinger and Thomas A. Harris [No. 387], p. 499
Wind tunnel tests on airfoil boundary layer control using a backward-opening slot, by Millard J. Bamber [No. 385], p. 439
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