Format:
Online-Ressource (582 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. 9003
Note:
A preliminary investigation of supercharging an air-cooled engine in flight, by Marsden Ware and Oscar W. Schey [No. 283], p. 81
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A study of wing flutter, by A.F. Zahm and R.M. Bear [No. 285], p. 107
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Aerodynamic characteristics of airfoils-V, by National Advisory Committee for Aeronautics [No. 286], p. 135
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Aircraft accidents, by Special Subcommittee of the National Advisory Committee for Aeronautics [No. 308], p. 557
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An investigation of the aerodynamic characteristics of an airplane equipped with several different sets of wings, by J.W. Crowley, Jr., and M.W. Green [No. 303], p. 477
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An investigation of the aerodynamic characteristics of an airplane equipped with several different sets of wings, by J.W. Crowley, Jr., and M.W. Green [No. 304], p. 487
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An investigation of the use of discharge valves and intake control for improving the performance of N.A.C.A. Roots Type Supercharger, by Oscar W. Schey and Ernest E. Wilson [No. 302], p. 477
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Characteristics of five propellers in flight, by J.W. Crowley, Jr., and R.E. Mixson [No. 292], p. 265
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Drag of C-class airship hulls of various fineness ratios, by A.F. Zahm, R.H. Smith, and F.A. Louden [No. 291], p. 249
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Effect of variation of chord and span of ailerons on rolling and yawing moments in level flight, by R.H. Heald and D.H. Strother [No. 298], p. 383
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Forces on elliptic cylinders in uniform air stream, by A.F. Zahm, R.H. Smith, and F.A. Louden [No. 289], p. 215
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Full scale tests on a thin metal propeller at various tip speeds, by Fred E. Weick [No. 301], p. 463
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Full-scale wind-tunnel tests of a series of metal propellers on a VE-7 airplane, by Fred E. Weick [No. 306], p. 519
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Investigation of damping liquids for aircraft instruments, by G.H. Keulegan [No. 299], p. 403
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Pressure distribution over a rectangular monoplane wing model up to 90' angle of attack, by Montgomery Knight and Ocsar Loeser, Jr. [No. 288], p. 195
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Pressure distribution tests on PW-9 models from -18' through 90' angle of attack, by Oscar E. Loeser, Jr. [No. 296], p. 333
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Reduction of observed airplane performance to standard conditions, by Walter S. Diehl [No. 297], p. 355
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Table of contents, p. VI
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The comparative performance of roots type aircraft engine superchargers as affected by change in impeller speed and displacement, by Marsden Ware and Ernest E. Wilson [No. 284], p. 93
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The gaseous explosive reaction: A study of the kinetics of composite fuels, by F.W. Stevens [No. 305], p. 501
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The measurement of maximum cylinder pressures, by Chester W. Hicks [No. 294], p. 309
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The pressure distribution over the horizontal and vertical tail surfaces of the F6C-4 pursuit airplane in violent maneuvers, by R.V. Rhode [No. 307], p. 537
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The twenty-foot propeller research tunnel of the National Advisory Committee for Aeronautics, by Fred E. Weick and Donald H. Wood [No. 300], p. 427
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The variation in engine power with altitude determined from measurements in flight with a hub dynamometer, by W.D. Gove [No. 295], p. 321
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Theories of flow similitude, by A.F. Zahm [No. 287], p. 185
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Two practical methods for the calculation of the horizontal tail area necessary for a statically stable airplane, by Walter S. Diehl [No. 293], p. 289
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Water-pressure distribution on a seaplane float, by F.L. Thompson [No. 290], p. 233
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