Aeronautics. Sixteenth annual report of the National Advisory Committee for Aeronautics, 1930, including technical reports Nos. 337 to 364.

Aeronautics. Sixteenth annual report of the National Advisory Committee for Aeronautics, 1930, including technical reports Nos. 337 to 364. [electronic resource]

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Bibliographic Details
Online Access:	Online Access
Corporate Authors:	United States. Congress. Senate, United States. President (1929-1933 : Hoover), United States. National Advisory Committee for Aeronautics
Other Authors:	Anderson, Raymond F., Black, Goldie A., Brombacher, W. G. (William George), 1891-, Brueggeman, W. C. (William Charles), Davis, Merlin, Dryden, Hugh L. (Hugh Latimer), 1898-1965, Durand, William Frederick, 1859-1958, Foster, H. H. (Hampton Hodge), 1894-, Harris, Thomas A., Heald, R.H, Hicks, Chester W., Hoover, Herbert, 1874-1964, Jacobs, Eastman N. (Eastman Nixon), 1902-1987, Joachim, W. F., Knight, Montgomery, 1901-1943, Kuethe, Arnold M. (Arnold Martin), 1905-, Markwardt, L. J. (Lorraine Joseph), 1889-, Melton, E. R. (Edward R.), Millikan, Clark Blanchard, 1903-1966, Monish, B .H, Newlin, J. A. (John A.), 1872-1943, Peters, Melville F., Pinkerton, Robert M., Rhode, Richard V., Rothrock, A. M. (Addison May), 1903-1971, Schey, Oscar W., Schuman, Louis, Stack, John, 1906-1972, Stevens, F. W., -1932, Strother, D. H. (David H.), Summerville, Wayne L., Thompson, F. L., Trayer, George W. (George William), 1888-1976, Weick, Fred E., Whittemore, Herbert L. (Herbert Lucius), 1876-, Wood, Donald H., Young, Alfred W.
Format:	Government Document Electronic eBook
Language:	English
Published:	Washington, DC, 1930.
Series:	United States congressional serial set ; serial set no. 9348. Senate document (United States. Congress. Senate) ; 71st Congress, no. 219.
Subjects:	United States. > National Advisory Committee for Aeronautics. Advisory boards. Aeronautics. Aircraft accidents and safety. Aircraft construction. Aircraft engines. Airplanes. Airships. Engineering. Internal combustion engines. Military aircraft. Technology. Transportation research. Transportation safety. Aircraft pilots. Annual Reports. Monographs. Presidential Communications and Messages.

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Item Description:	Table of contents, p. VI. List of technical reports, p. VII. The gaseous explosive reaction at constant pressure -- the reaction order and reaction rate, by F.W. Stevens [No. 337], p. 67. The effect of reduction gearing on propeller-body interference as shown by full scale wind tunnel tests, by Fred E. Weick [No. 338], p. 83. Full scale wind tunnel tests with a series of propellers of different diameters on a single fuselage, by Fred E. Weick [No. 339], p. 105. Full scale wind tunnel tests on several metal propellers having different blade forms, by Fred E. Weick [No. 340], p. 121. The design and development of an automatic injection valve with an annular orifice of varying area, by William F. Joachim, Chester W. Hicks, and Hampton H. Foster [No. 341], p. 135. Effect of turbulence in wind tunnel measurements, by H.L. Dryden and A.M. Kuethe [No. 342], p. 145. Effect of variation of chord and span of ailerons on rolling and yawing moments at several angles of pitch, by R.H. Heald, D.H. Strother, and B.H. Monish [No. 343], p. 171. The design of plywood webs for airplane wing beams, by George W. Trayer [No. 344], p. 201. The design of airplane wing ribs, by J.A. Newlin and George W. Trayer [No. 345], p. 219. Water pressure distribution on a flying boat hull, by F.L. Thompson [No. 346], p. 273. A method of calculating the ultimate strength of continuous beams, by J.A. Newlin and George W. Trayer [No. 347], p. 291. Strength of welded joints in tubular members for aircraft, by H.L. Whittemore and W.C. Brueggeman [No. 348], p. 319. A proof of the theorem regarding the distribution of lift over the span for minimum induced drag, by W.F. Durand [No. 349], p. 361. Working charts for the selection of aluminum alloy propellers of a standard form to operate with various aircraft engines and bodies, by Fred E. Weick [No. 350], p. 377. Full scale wind tunnel tests of a propeller with the diameter changed by cutting off the blade tips, by Donald H. Wood [No. 351], p. 393. Large scale aerodynamic characteristics of airfoils as tested in the variable density wind tunnel, by Eastman N. Jacobs and Raymond F. Anderson [No. 352], p. 419. Airfoil pressure distribution investigation in the variable density wind tunnel, by Eastman N. Jacobs, John Stack, and Robert M. Pinkerton [No. 353], p. 451. Aircraft woods: Their properties, selection, and characteristics, by L.J. Markwardt [No. 354], p. 467. Comparative flight performance with an N.A.C.A. roots supercharger and a turbocentrifugal supercharger, by Oscar W. Schey and Alfred W. Young [No. 355], p. 501. Strength of rectangular flat plates under edge compression, by Louis Schuman and Goldie Black [No. 356], p. 515. Aircraft accidents: Method of analysis, by Committee on Aircraft Accidents of the National Advisory Committee for Aeronautics [No. 357], p. 539. Temperature coefficient of the modulus of rigidity of aircraft instrument diaphragm and spring materials, by W.G. Brombacher and E.R. Melton [No. 358], p. 557. An investigation of the effectiveness of ignition sparks, by Melville F. Peters, Wayne L. Summerville, and Merlin Davis [No. 359], p. 573. Pressure distribution over a symmetrical airfoil section with trailing edge flap, by Eastman N. Jacobs and Robert M. Pinkerton [No. 360], p. 587. Experimental determination of jet boundary corrections for airfoil tests in four open wind tunnel jets of different shapes, by Montgomery Knight and Thomas A. Harris [No. 361], p. 607. An extended theory of thin airfoils and its application to the biplane problem, by Clark B. Millikan [No. 362], p. 635. Pressure fluctuations in a common-rail fuel injection system, by A.M. Rothrock [No. 363], p. 669. The pressure distribution over the wings and tail surfaces of a PW-9 pursuit airplane in flight, by Richard V. Rhode [No. 364], p. 685.
Physical Description:	799 p. : illustrations, tables.