Format:
Online-Ressource (799 p)
,
illustrations, tables
Edition:
Online-Ausg. Chester, Vt NewsBank, inc 2007 U.S. Congressional Serial Set, 1817-1980
Series Statement:
United States congressional serial set serial set no. 9348
Note:
A method of calculating the ultimate strength of continuous beams, by J.A. Newlin and George W. Trayer [No. 347], p. 291
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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
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Aircraft accidents: Method of analysis, by Committee on Aircraft Accidents of the National Advisory Committee for Aeronautics [No. 357], p. 539
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Aircraft woods: Their properties, selection, and characteristics, by L.J. Markwardt [No. 354], p. 467
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Airfoil pressure distribution investigation in the variable density wind tunnel, by Eastman N. Jacobs, John Stack, and Robert M. Pinkerton [No. 353], p. 451
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An extended theory of thin airfoils and its application to the biplane problem, by Clark B. Millikan [No. 362], p. 635
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An investigation of the effectiveness of ignition sparks, by Melville F. Peters, Wayne L. Summerville, and Merlin Davis [No. 359], p. 573
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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
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Effect of turbulence in wind tunnel measurements, by H.L. Dryden and A.M. Kuethe [No. 342], p. 145
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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
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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
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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
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Full scale wind tunnel tests on several metal propellers having different blade forms, by Fred E. Weick [No. 340], p. 121
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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
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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
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List of technical reports, p. VII
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Pressure distribution over a symmetrical airfoil section with trailing edge flap, by Eastman N. Jacobs and Robert M. Pinkerton [No. 360], p. 587
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Pressure fluctuations in a common-rail fuel injection system, by A.M. Rothrock [No. 363], p. 669
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Strength of rectangular flat plates under edge compression, by Louis Schuman and Goldie Black [No. 356], p. 515
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Strength of welded joints in tubular members for aircraft, by H.L. Whittemore and W.C. Brueggeman [No. 348], p. 319
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Table of contents, p. VI
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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
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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
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The design of airplane wing ribs, by J.A. Newlin and George W. Trayer [No. 345], p. 219
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The design of plywood webs for airplane wing beams, by George W. Trayer [No. 344], p. 201
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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
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The gaseous explosive reaction at constant pressure -- the reaction order and reaction rate, by F.W. Stevens [No. 337], p. 67
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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
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Water pressure distribution on a flying boat hull, by F.L. Thompson [No. 346], p. 273
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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
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