Report. Aeronautics, 17th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1931, including Technical reports 365-400.
Publication Title:
Report. Aeronautics, 17th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1931, including Technical reports 365-400.
Display Title:
Report. Aeronautics, 17th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1931, including Technical reports 365-400.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Date:
1932
Publish Date ISO Format:
1932-01-01T00:00:00Z
Publication Start:
19320101
Publication End:
19321231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
13
Publication year:
1932
SuDoc number:
Y 3.N 21/5:1/931-2
Description:
viii+722 p. il. 4°
Notes:
[Each report is also published separately in advance.]
Notes:
[Each report is also published separately in advance.] * For Sale by Superintendent of Documents. Cloth, $3.00.
Notes:
CONTENTS.—17th annual report.—Report 365. Aerodynamic characteristics of circular-arc airfoils at high speeds; by L. J. Briggs and H. L. Dryden.—Report 366. Dynamic and flight tests on rubber-cord and oleo-rubber-disk landing gears for F6C-4 airplane [with references and bibliography]; by William C. Peck.—Report 367. Pressure distribution over thick, tapered and twisted monoplane wine model, N. A. C. A. 81-J [with list of references]; by Carl J. Wenzinger.—Report 368. New chart for estimating absolute ceiling of airplane [with list of references]; by Walter S. Diehl.—Report 369. Maneuverability investigation of F6C-3 airplane with special flight instruments [with references and bibliography]; by C. H. Dearborn and H. W. Kirschbaum.—Report 370. Effect of variation of chord and span of ailerons on hinge moments at several angles of pitch [with list of references]; by B. H. Monish.—Report 371. Present status of aircraft instruments [with list of references]; report prepared by Subcommittee on Instruments.—Report 372. Gaseous explosive reaction, effect of pressure on rate of propagation of reaction zone and upon rate of molecular transformation [with list of references]; by F. W. Stevens.—Report 373. Coefficients of discharge of fuel injection nozzles for compression-ignition engines [with list of references]; by A. G. Gelalles.—Report 374. Automotive ignition coil [with list of references]; by T. H. Darnell.—Report 375. Full-scale tests of metal propellers at high tip speeds [with list of references]; by Donald H. Wood.—Report 376. Some approximate equations for standard atmosphere; by Walter S. Diehl.—Report 377. Method of flight measurement of spins [with list of references]; by Hartley A. Soulé and Nathan F. Scudder.—Report 378. Comparison of full-scale propellers having R. A. F.-6 and dark Y airfoil sections [with list of references]; by Hugh B. Freeman.—Report 379. Rolling moments due to rolling and yaw for 4 wing models in rotation [with list of references]; by Montgomery Knight and Carl J. Wenzinger.—Report 380. Pressure distribution over fuselage of PW-9 pursuit airplane in flight [with list of references]; by Richard V. Rhode and Eugene E. Lundquist.—Report 381. Static, drop, and flight tests on Musselman type airwheels [with list of references]; by William C. Peck and Albert P. Beard.—Report 382. Elastic instability of members having sections common in aircraft construction [with list of references]; by George W. Trayer and H. W. March.—Report 383. On theory of wing sections with particular reference to lift distribution [with list of references]; by Theodore Theodorsen.—Report 384. Comparative performance of superchargers [with list of references]; by Oscar W. Schey.—Report 385. Wind-tunnel tests on airfoil boundary layer control using backward-opening slot [with list of references]; by Millard J. Bamber.—Report 386. Maneuverability investigation of F6C-4 fighting airplane [with references and bibliography]; by C. H. Dearborn and H. W. Kirschbaum.—Report 387. Vertical wind tunnel of National Advisory Committee for Aeronautics [with list of references]; by Carl J. Wenzinger and Thomas A. Harris.—Report 388. Investigation of diaphragm-type pressure cell [with list of references]; by Theodore Theodorsen.—Report 389. Effect of small angles of yaw and pitch on characteristics of airplane propellers [with references and bibliography]; by Hugh B. Freeman.—Report 390. Effect of valve timing upon performance of supercharged engine at altitude and unsupercharged engine at sea level [with references and bibliography]; by Oscar W. Schey and Arnold E. Biermann.—Report 391. Aerodynamic characteristics of 8 very thick airfoils from tests in variable density wind tunnel [with list of reference]; by Eastman N. Jacobs.—Report 392. Reduction of turbulence in wind tunnels [with list of references]; by Hugh L. Dryden.—Report 393. Span-load distribution as factor in stability in roll [with list of references]; by Montgomery Knight and Richard W. Noyes.—Report 394. Airship model tests in variable density wind tunnel [with list of references]; by Ira H. Abbott.—Report 395. New principle of sound frequency analysis [with list of references]; by Theodore Theodorsen.—Report 396. Hydraulics of fuel injection pumps for compression ignition engines [with list of references]; by A. M. Rothrock.—Report 397. Drag characteristics of several airships determined by deceleration tests [with list of references]; by F. L. Thompson and H. W. Kirschbaum.—Report 398. Investigation of damping liquids for aircraft instruments, 2 (with list of references]; by M. R. Houseman and G. H. Keulegan.—Report 399. Flame movement and pressure development in engine cylinder [with list of references]; by Charles F. Marvin, jr., and Robert D. Best.—Report 400. Aerodynamic characteristics of slotted Clark Y wing as affected by auxiliary airfoil position [with list of references]; by Carl J. Wenzinger and Joseph A. Shortal.—Aeronautical symbols.
Availability:
* For Sale by Superintendent of Documents. Cloth, $3.00.