Format:
Online-Ressource (756 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. 9667
Note:
A method for computing leading-edge loads, by Richard V. Rhode and Henry A. Pearson [No. 413], p. 249
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Aircraft speed instruments, by K. Hilding Beij [No. 420], p. 381
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Appendix, p. 237
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Application of practical hydrodynamics to airship design, by Ralph H. Upson and W.A. Klikoff [No. 405], p. 123
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Characteristics of Clark Y airfoils of small aspect ratios, by C.H. Zimmerman [No. 431], p. 581
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Combustion in a high-speed compression-ignited engine, by A.M. Rothrock [No. 401], p. 63
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Drop and flight tests on NY-2 landing gears including measurements of vertical velocities at landing, by W.C. Peck and A.P. Beard [No. 406], p. 141
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Effect of orifice length-diameter ratio on fuel sprays for compression-ignition engines, by A.G. Gelalles [No. 402], p. 79
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Experiments on the distribution of fuel in fuel sprays, by Dana W. Lee [No. 438], p. 703
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Force measurements on a 1/40-scale model of the U.S. airship Akron, by Hugh B. Freeman [No. 432], p. 591
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Fuel vaporization and its effect on combustion in a high-speed compression-ignition engine, by A.M. Rothrock and C.D. Waldron [No. 435], p. 629
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General formulas and charts for the calculation of airplane performance, by W. Bailey Oswald [No. 408], p. 163
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Ice prevention on aircraft by means of engine exhaust heat and a technical study of heat transmission from a Clark Y airfoil, by Theodore Theodorsen and William C. Clay [No. 403], p. 91
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Lift and drag characteristics and gliding performance of an autogiro as determined in flight, by John B. Wheatley [No. 434], p. 621
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Measurement of the differential and total thrust and torque of six full-scale adjustable-pitch propellers, by George W. Stickle [No. 421], p. 437
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Measurements of flow in the boundary layer of a 1/40-scale model of the U.S. airship Akron, by Hugh B. Freeman [No. 430], p. 567
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Preliminary investigation of modifications to conventional airplanes to give nonstalling and short-landing characteristics, by Fred E. Weick [No. 418], p. 343
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Pressure distribution tests on a series of Clark Y biplane cellules with special reference to stability, by Richard W. Noyes [No. 417], p. 315
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Rates of fuel discharge as affected by the design of fuel-injection systems for internal-combustion engines, by A.G. Gelalles and E.T. Marsh [No. 433], p. 607
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Table of contents, p. VII
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Tests of nacelle-propeller combinations in various positions with reference to wings. Part I. Thick wing -- N.A.C.A. cowled nacelle-tractor propeller, by Donald H. Wood [No. 415], p. 277
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Tests on nacelle-propeller combinations in various positions with reference to wings. II. -- Thick wing -- various radial-engine cowlings -- tractor propeller, by Donald H. Wood [No. 436], p. 653
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The 7 by 10 foot wind tunnel of the National Advisory Committee for Aeronautics, by Thomas A. Harris [No. 412], p. 241
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The N.A.C.A. apparatus for studying the formation and combustion of fuel sprays and the results from preliminary tests, by A.M. Rothrock [No. 429], p. 549
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The N.A.C.A. variable-density wind tunnel, by Eastman N. Jacobs and Ira H. Abbott [No. 416], p. 305
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The characteristics of a Clark Y wing model equipped with several forms of low-drag fixed slots, by Fred E. Weick and Carl J. Wenzinger [No. 407], p. 155
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The effect of area and aspect ratio on the yawing moments of rudders at large angles of pitch on three fuselages, by Hugh L. Dryden and B.H. Monish [No. 437], p. 693
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The effect of humidity on engine power at altitude, by D.B. Brooks and E.Z. Garlock [No. 426], p. 523
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The effect of increased carburetor pressure on engine performance at several compression ratios, by Oscar W. Schey and Vern G. Rollin [No. 404], p. 113
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The effect of multiple fixed slots and a trailing-edge flap on the lift and drag of a Clark Y airfoil, by Fred E. Weick and Joseph A. Shortal [No. 427], p. 531
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The effect of nozzle design and operating conditions on the atomization and distribution of fuel sprays, by Dana W. Lee [No. 425], p. 505
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The effect on airplane performance of the factors that must be considered in applying low-drag cowling to radial engines, by William H. McAvoy, Oscar W. Schey, and Alfred W. Young [No. 414], p. 259
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The elimination of fire hazard due to back fires, by Theodore Theodorsen and Ira M. Freeman [No. 409], p. 211
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The mechanism of atomization accompanying solid injection, by R.A. Castleman, Jr. [No. 440], p. 735
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The theory of wind-tunnel wall interference, by Theodore Theodorsen [No. 410], p. 219
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Theory of wing sections of arbitrary shape, by Theodore Theodorsen [No. 411], p. 229
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Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. I. -- Ordinary ailerons on rectangular wings, by Fred E. Weick and Carl J. Wenzinger [No. 419], p. 357
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Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. II. -- Slotted ailerons and Frise ailerons, by Fred E. Weick and Richard W. Noyes [No. 422], p. 457
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Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. III. -- Ordinary ailerons rigged up 10 [degrees] when neutral, by Fred E. Weick and Carl J. Wenzinger [No. 423], p. 471
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Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. IV. -- Floating tip ailerons on rectangular wings, by Fred E. Weick and Thomas A. Harris [No. 424], p. 481
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Wind-tunnel research comparing lateral control devices, particularly at high angles of attack. V. -- Spoilers and ailerons on rectangular wings, Fred E. Weick and Joseph A. Shortal [No. 439], p. 719
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Wind-tunnel tests of a Clark Y wing with a narrow auxiliary airfoil in different positions, by Fred E. Weick and Millard J. Bamber [No. 428], p. 537
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