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Format: Online-Ressource (730 p) , illustrations, maps, 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. 9523

Note: A method of flight measurement of spins, by Hartley A. Soule and Nathan F. Scudder [No. 377], p. 267 , A new chart for estimating the absolute ceiling of an airplane, by Walter S. Diehl [No. 368], p. 111 , A new principle of sound frequency analysis, by Theodore Theodorsen [No. 395], p. 605 , Aerodynamic characteristics of circular-arc airfoils at high speeds, by L.J. Briggs and H.L. Dryden [No. 365], p. 67 , Airship model tests in the variable density wind tunnel, by Ira H. Abbott [No. 394], p. 583 , Coefficients of discharge of fuel injection nozzles for compression-ignition engines, by A.G. Gelalles [ No. 373], p. 193 , Comparison of full-scale propellers having R.A.F.-6 and Clark Y airfoil sections, by Hugh B. Freeman [No. 378], p. 283 , Dynamic and flight tests on rubber-cord and oleo-rubber-disk landing gears for an F6C-4 airplane, by William C. Peck [No. 366], p. 79 , Effect of variation of chord and span of ailerons on hinge moments at several angles of pitch, by B.H. Monish [No. 370], p. 137 , Elastic instability of members having sections common in aircraft construction, by George W. Trayer and H.W. March [No. 382], p. 373 , Flame movement and pressure development in an engine cylinder, by Charles F. Marvin, Jr., and Robert D. Best [No. 399], p. 697 , Full-scale tests of metal propellers at high tip speeds, by Donald H. Wood [No. 375], p. 237 , Hydraulics of fuel injection pumps for compression-ignition engines, by A.M. Rothrock [No. 396], p. 621 , Investigation of damping liquids for aircraft instruments -- II, by M.R. Houseman and G.H. Keulegan [No. 398], p. 679 , Investigation of the diaphragm-type pressure cell, by Theodore Theodorsen [No. 388], p. 507 , Maneuverability investigation of an F6C-4 fighting airplane, by C.H. Dearborn and H.W. Kirschbaum [No. 386], p. 475 , Maneuverability investigation of the F6C-3 airplane with special flight instruments, by C.H. Dearborn and H.W. Kirschbaum [No. 369], p. 117 , On the theory of wing sections with particular reference to the lift distribution, by Theodore Theodorsen [No. 383], p. 411 , Present status of aircraft instruments, by Subcommittee on Instruments [No. 371], p. 153 , Pressure distribution over a thick, tapered and twisted monoplane wing model -- N.A.C.A. 81 J, by Carl J. Wenzinger [No. 367], p. 97 , Pressure distribution over the fuselage of a PW-9 pursuit airplane in flight, by Richard V. Rhode and Eugene E. Lundquist [No. 380], p. 327 , Reduction of turbulence in wind tunnels, by Hugh L. Dryden [No. 392], p. 557 , Rolling moments due to rolling and yaw for four wing models in rotation, by Montgomery Knight and Carl J. Wenzinger [No. 379], p. 301 , Some approximate equations for the standard atmosphere, by Walter S. Diehl [No. 376], p. 257 , Span-load distribution as a factor in stability in roll, by Montgomery Knight and Richard W. Noyes [No. 393], p. 567 , Static, drop, and flight tests on Musselman type airwheels, by William C. Peck and Albert P. Beard [No. 381], p. 355 , Table of contents, p. VI , The aerodynamic characteristics of a slotted Clark Y wing as affected by the auxiliary airfoil position, by Carl J. Wenzinger and Joseph A. Shortal [No. 400], p. 707 , The aerodynamic characteristics of eight very thick airfoils from tests in the variable density wind tunnel, by Eastman N. Jacobs [No. 391], p. 545 , The automotive ignition coil, by T.H. Darnell [No. 374], p. 211 , The comparative performance of superchargers, by Oscar W. Schey [No. 384], p. 425 , The drag characteristics of several airships determined by deceleration tests, by F.J. Thompson and H.W. Kirschbaum [No. 397], p. 665 , The effect of small angles of yaw and pitch on the characteristics of airplane propellers, by Hugh B. Freeman [No. 389], p. 523 , The effect of valve timing upon the performance of a supercharged engine at altitude and an unsupercharged engine at sea level, by Oscar W. Schey and Arnold E. Biermann [No. 390], p. 533 , The gaseous explosive reaction -- the effect of pressure on the rate of propagation of the reaction zone and upon the rate of molecular transformation, by F.W. Stevens [No. 372], p. 175 , The vertical wind tunnel of the National Advisory Committee for Aeronautics, by Carl J. Wenzinger and Thomas A. Harris [No. 387], p. 499 , Wind tunnel tests on airfoil boundary layer control using a backward-opening slot, by Millard J. Bamber [No. 385], p. 439 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (645 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. 9802

Note: A comparison between the theoretical and measured longitudinal stability characteristics of an airplane, by Hartley A. Soule and John B. Wheatley [No. 442], p. 53 , A flight investigation of the spinning of the NY-1 airplane with varied mass distribution and other modifications, and an analysis based on wind-tunnel tests, by Nathan F. Schudder [No. 441], p. 37 , Aircraft power-plant instruments, by Harcourt Sontag and W.G. Brombacher [No. 466], p. 447 , Airfoil section characteristics as affected by protuberances, by Eastman N. Jacobs [No. 446], p. 109 , Appendix, p. 65 , Determination of the theoretical pressure distribution for twenty airfoils, by I.E. Garrick [No. 465], p. 433 , General potential theory of arbitrary wing sections, by T. Theodorsen and I.E. Garrick [No. 452], p. 177 , Improved apparatus for the measurement of fluctuations of air speed in turbulent flow, by W.C. Mock, Jr. and H.L. Dryden [No. 448], p. 131 , Increasing the air charge and scavenging the clearance volume of a compression-ignition engine, by J.S. Spanogle, C.W. Hicks, and H.H. Foster [No. 469], p. 525 , Interference on an airfoil of finite span in an open rectangular wind tunnel, by Theodore Theodoresen [No. 561], p. 355 , List of technical reports, p. VII , Maneuverability investigation of O3U-1 observation airplane, by F.L. Thompson and H.W. Kirschbaum [No. 457], p. 263 , Negative thrust and torque characteristics of an adjustable-pitch metal propeller, by Edwin P. Hartmen [No 464], p. 421 , Nomenclature for aeronautics, by National Advisory Committee for Aeronautics [No. 474], p. 603 , Penetration and duration of fuel sprays from a pump injection system, by A.M. Rothrock and E.T. March [No. 455], p. 241 , Performance of a fuel-injection spark-ignition engine using a hydrogenated safety fuel, by Oscar W. Schey and Alfred W. Young [No. 471], p. 557 , Photomicrographic studies of fuel sprays, by Dana W. Lee and Robert C. Spencer [No. 454], p. 215 , Pressure-distribution measurements on the hull and fins of a 1/40-scale model of the U.S. airship Akron, by Hugh B. Freeman [No. 443], p. 67 , Relative loading on biplane wings, by Walter S. Diehl [No. 458], p. 275 , Static thrust of airplane propellers, by Walter S. Diehl [No. 447], p. 125 , Strength tests of thin-walled duralumin cylinders in compression, by Eugene E. Lundquist [No. 473], p. 585 , Tests of nacelle-propeller combinations in various positions with reference to wings. III. -- Clark Y wing -- Various radial-engine cowlings -- Tractor propeller, by Donald H. Wood [No. 462], p. 359 , The N.A.C.A. full-scale wind tunnel, by Smith J. De France [No. 459], p. 291 , The N.A.C.A. high-speed wind tunnel and tests of six propeller sections, by John Stack [No. 463], p. 399 , The N.A.C.A. tank: A high-speed towing basin for testing models of seaplane floats, by Starr Truscott [No. 470], p. 535 , The aerodynamic forces and moments exerted on a spinning model of the NY-1 airplane as measured by the spinning balance, by M.J. Bamber and C.H. Zimmerman [No. 456], p. 249 , The calculation of take-off run, by Walter S. Diehl [No. 450], p. 163 , The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel, by Eastman N. Jacobs, Kenneth E. Ward, and Robert M. Pinkerton [No. 460], p. 299 , The drag of two streamline bodies as affected by protuberances and appendages, by Ira H. Abbot [No. 451], p. 171 , The estimation of maximum load capacity of seaplanes and flying boats, by Walter S. Diehl [No. 453], p. 211 , The experimental determination of the moments of inertia of airplanes, by Hartley A. Soule and Marvel P. Miller [No. 467], p. 501 , The interference between struts in various combinations, by David Biermann and William H. Herrnstein, Jr. [No. 468], p. 515 , Wind-tunnel research comparing lateral control devices particularly at high angles of attack. VI. -- Skewed ailerons and rectangular wings, by Fred E. Weick and Thomas A. Harris [No. 444], p. 81 , Wind-tunnel tests on combinations of a wing with fixed auxiliary airfoils having various chords and profiles, by Fred E. Weick and Robert Sanders [No. 472], p. 567 , Wing characteristics as affected by protuberances of short span, by Eastman N. Jacobs and Albert Sherman [No. 449], p. 155 , Working charts for the determination of the lift distribution between biplane wings, by Paul Kuhn [No. 445], p. 93 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)