Report. Aeronautics, 16th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1930, including Technical reports 337-364.
Publication Title:
Report. Aeronautics, 16th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1930, including Technical reports 337-364.
Display Title:
Report. Aeronautics, 16th annual report of National Advisory Committee for Aeronautics, [fiscal year] 1930, including Technical reports 337-364.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Date:
1931
Publish Date ISO Format:
1931-01-01T00:00:00Z
Publication Start:
19310101
Publication End:
19311231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
13
Publication year:
1931
SuDoc number:
Y 3.N 21/5:1/930-2
Description:
viii+787 p. il. 2 pl. 2 p. of pl. 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.—16th annual report.—Report 337. Gaseous explosive reaction at constant pressure, reaction order and reaction rate [with list of references]; by F. W. Stevens.—Report 338. Effect of reduction gearing on propeller-body interference as shown by full scale wind tunnel tests [with list of references]; by Fred E. Weick.— Report 339. Full scale wind tunnel tests with series of propellers of different diameters on single fuselage [with reference]; by Fred E. Weick.—Report 340. Full scale wind tunnel tests on several metal propellers having different blade forms [with list of references]; by Fred E. Weick.—Report 341. Design and development of automatic injection valve with annular orifice of varying area [with bibliography]; by William F. Joachim, Chester W. Hicks, and Hampton H. Foster.—Report 342. Effect of turbulence in wind tunnel measurements [with list of references]; by H. L. Dryden and A. M. Kuethe.—Report 343. Effect of variation of chord and span of ailerons on rolling and yawing moments at several angles of pitch [with list of references]; by R. H. Heald, D. H. Strother, and B. H. Monish.—Report 344. Design of plywood webs for airplane wing beams; by George W. Trayer.—Report 345. Design of airplane wing ribs; by J. A. Newlin and Geo. W. Trayer.—Report 346. Water pressure distribution on flying boat hull [with references and bibliography]; by F. L. Thompson-Report 347. Method of calculating ultimate strength of continuous beams; by J. A. Newlin and Geo. W. Trayer.—Report 348. Strength of welded joints and tubular members for aircraft [with bibliography]; by H. L. Whittemore and W. C. Brueggeman.—Report 349. Proof of theorem regarding distribution of lift over span for minimum induced drag [with list of references]; by W. F. Durand.—Report 350. Working charts for selection of aluminum alloy propellers of standard form to operate with various aircraft engines and bodies [with list of references]; by Fred E. Weick.— Report 351. Full scale wind tunnel tests of propeller with diameter changed by cutting off blade tips [with list of references]; by Donald H. Wood.—Report 352. Largescale aerodynamic characteristics of airfoils as tested in variable density wind tunnel [with list of references]; by Eastman N. Jacobs and Raymond F. Anderson.—Report 353. Airfoil pressure distribution investigation in variable density wind tunnel [with list of references]; by Eastman N. Jacobs, John Stack, and Robert M. Pinkerton.— Report 354. Aircraft woods, their properties, selection, and characteristics [with list of references and bibliography]; by L. J. Markwardt.—Report 355. Comparative flight performance with N. A. C. A. Roots supercharger and turbocentrifugal supercharger [with list of references]; by Oscar W. Schey and Alfred W. Young.—Report 356. Strength of rectangular flat plates under edge compression; by Louis Schuman and Goldie Back.—Report 357. Aircraft accidents, method of analysis; report preparedby Committee on Aircraft Accidents.—Report 358. Temperature coefficient or modulus of rigidity of aircraft instrument diaphragm and spring materials [with list of references]; by W. G. Brombacher and E. R. Melton.—Report 359. Investigation of effectiveness of ignition sparks [with list of references]; by Melville F. Peters, Wayne L. Summerville, and Merlin Davis.—Report 360. Pressure distribution over symmetrical airfoil section with trailing edge flap [with list of references]; by Eastman N. Jacobs and Robert M. Pinkerton.—Report 361. Experimental determination of jet boundary corrections for airfoil tests in 4 open wind tunnel jets of different shapes [with list of references]; by Montgomery Knight and Thomas A. Harris.—Report 362. Extended theory of thin airfoils and its application to biplane problem [with list of references]; by Clark B. Millikan.—Report 363. Pressure fluctuations in common-rail fuel injection system [with list of references]; by A. M. Rothrock.—Report 364. Pressure distribution over wings and tail surfaces of PW-9 pursuit airplane in flight [with bibliography]; by Richard V. Rhode.
Availability:
* For Sale by Superintendent of Documents. Cloth, $3.00.