Kooperativer Bibliotheksverbund

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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 , A study of wing flutter, by A.F. Zahm and R.M. Bear [No. 285], p. 107 , Aerodynamic characteristics of airfoils-V, by National Advisory Committee for Aeronautics [No. 286], p. 135 , Aircraft accidents, by Special Subcommittee of the National Advisory Committee for Aeronautics [No. 308], p. 557 , 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 , 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 , 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 , Characteristics of five propellers in flight, by J.W. Crowley, Jr., and R.E. Mixson [No. 292], p. 265 , 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 , 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 , Forces on elliptic cylinders in uniform air stream, by A.F. Zahm, R.H. Smith, and F.A. Louden [No. 289], p. 215 , Full scale tests on a thin metal propeller at various tip speeds, by Fred E. Weick [No. 301], p. 463 , Full-scale wind-tunnel tests of a series of metal propellers on a VE-7 airplane, by Fred E. Weick [No. 306], p. 519 , Investigation of damping liquids for aircraft instruments, by G.H. Keulegan [No. 299], p. 403 , 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 , Pressure distribution tests on PW-9 models from -18' through 90' angle of attack, by Oscar E. Loeser, Jr. [No. 296], p. 333 , Reduction of observed airplane performance to standard conditions, by Walter S. Diehl [No. 297], p. 355 , Table of contents, p. VI , 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 , The gaseous explosive reaction: A study of the kinetics of composite fuels, by F.W. Stevens [No. 305], p. 501 , The measurement of maximum cylinder pressures, by Chester W. Hicks [No. 294], p. 309 , 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 , 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 , The variation in engine power with altitude determined from measurements in flight with a hub dynamometer, by W.D. Gove [No. 295], p. 321 , Theories of flow similitude, by A.F. Zahm [No. 287], p. 185 , 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 , Water-pressure distribution on a seaplane float, by F.L. Thompson [No. 290], p. 233 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (640 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. 8715

Note: A comparison of the take off and landing characteristics of a number of service airplanes, by Thomas Carroll, p. 455 , A preliminary study of fuel injection and compression ignition as applied to an aircraft engine cylinder, by Arthur W. Gardiner, p. 311 , Aerodynamic characteristics of airfoils-IV, by National Advisory Committee for Aeronautics, p. 327 , Approximations for column effect in airplane wing spars, by Edward P. Warner and Mac Short, p. 483 , Characteristics of a twin-float seaplane during take off, by John W. Crowley, Jr., and K.M. Ronan, p. 297 , Description of the N.A.C.A. universal test engine and some test results, by Marsden Ware, p. 467 , Distribution of pressure over model of the upper wing and aileron of a Fokker D-VII airplane, by A.J. Fairbanks, p. 539 , Electrical characteristics of spark generators for automotive ignition, by R.B. Brode, D.W. Randolph, and F.B. Silsbee, p. 267 , Flow and drag formulas for simple quadrics, by A.F. Zahm, p. 515 , Interaction between air propellers and airplane structures, by W.F. Durand, p. 105 , Meteorological conditions along airways, by W.R. Gregg, p. 369 , Nomenclature for aeronautics, by National Advisory Committee for Aeronautics, p. 191 , Power output and air requirements of a two-stroke cycle engine for aeronautical use, by C.R. Paton and Carlton Kemper, p. 179 , Pressure distribution over airfoils at high speeds, by L.J. Briggs and H.L. Dryden, p. 553 , Pressure of air on coming to rest from various speeds, by A.F. Zahm, p. 409 , Table of contents, p. VII , Tables for calibrating altimeters and computing altitudes based on the standard atmosphere, by W.G. Brombacher, p. 385 , Tests on airplane fuselages, floats, and hulls, by Walter S. Diehl, p. 129 , Tests on thirteen navy type model propellers, by W.F. Durand, p. 151 , The aerodynamic characteristics of seven frequently used wing sections at full Reynolds number, by Max M. Munk and Elton W. Miller, p. 71 , The air forces on a systematic series of biplane and triplane cellule models, by Max M. Munk, p. 595 , The corrosion of magnesium and of the magnesium aluminum alloys containing manganese, J.A. Boyer, p. 417 , The direct measurement of engine power on an airplane in flight with a hub type dynamometer, by W.D. Gove and M.W. Green, p. 503 , The effects of flight path inclination on airplane velocity, by Walter S. Diehl, p. 167 , Three methods of calculating range and endurance of airplanes, by Walter S. Diehl, p. 87 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (787 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. 9221

Note: Table of contents, p. VI , Table of technical reports, p. VII , Technical Report No. 309. Joint report on standardization tests on N.P.L. R.A.F. 15 Airfoil Model, by Walter S. Diehl, p. 91 , Technical Report No. 310. Pressure element of constant logarithmic stiffness for temperature compensated altimeter, by W.G. Brombacher and F. Cordero, p. 111 , Technical Report No. 311. Aerodynamic theory and test of strut forms, by R.H. Smith, p. 125 , Technical Report No. 312. The prediction of airfoil characteristics, by George J. Higgins, p. 149 , Technical Report No. 313. Drag and cooling with various forms of cowling for a "Whirlwind" radial air-cooled engine-I, by Fred E. Weick, p. 163 , Technical Report No. 314. Drag and cooling with various forms of cowling for a "Whirlwind" radial air-cooled engine-II, by Fred E. Weick, p. 189 , Technical Report No. 315. Aerodynamic characteristics of airfoils-VI, by National Advisory Committee for Aeronautics, p. 211 , Technical Report No. 316. Tables for pressure of air coming to rest from various speeds, by A.F. Zahm and F.A. Louden, p. 247 , Technical Report No. 317. Wind tunnel tests on a series of wing models through a large angle of attack range. Part I -- Force tests, by Montgomery Knight and Carl J. Wenzinger, p. 255 , Technical Report No. 318. Speed and deceleration trials of U.S.S. Los Angeles, by S.J. DeFrance and C.P. Burgess, p. 305 , Technical Report No. 319. Aerodynamic characteristics of twenty-four air-foils at high speed, by L.J. Briggs and H.L. Dryden, p. 325 , Technical Report No. 320. The measurement of fluctuations of air speed by hot-wire anemometer, by H.L. Dryden and A.M. Kuethe, p. 357 , Technical Report No. 321. Fuel vapor pressures and the relation of vapor pressure to the preparation of fuel for combustion in fuel injection engines, by William F. Joachim and A.M. Rothrock, p. 383 , Technical Report No. 322. Investigation of air flow in open-throat wind tunnels, by Eastman N. Jacobs, p. 397 , Technical Report No. 323. Flow and force equations for a body revolving in fluid, by A.F. Zahm, p. 409 , Technical Report No. 324. Flight tests on U.S.S. Los Angeles. Part I. -- Full scale pressure distribution investigation, by S.J. DeFrance, p. 449 , Technical Report No. 325. Flight tests on U.S.S. Los Angeles. Part II. -- Stress and strength determination, by C.P. Burgess, p. 483 , Technical Report No. 326. Tests of five metal model propellers with various pitch distributions in a free wind stream and in combination with a model VE-7 fuselage, by E.P. Lesley and Elliott G. Reid, p. 499 , Technical Report No. 327. The effect of supercharger capacity on engine and airplane performance, by O.W. Schey and W.D. Gove, p. 517 , Technical Report No. 328. Water pressure distribution on a twin-float seaplane, by F.L. Thompson, p. 537 , Technical Report No. 329. The torsional strength of wings, by C.P. Burgess, p. 555 , Technical Report No. 330. Experimental and analytical determination of the motion of hydraulically operated valve stems in oil engine injection systems, by A.G. Gelalles and A.M. Rothrock, p. 569 , Technical Report No. 331. Collection of wind-tunnel data on commonly used wing sections, by F.A. Louden, p. 589 , Technical Report No. 332. The effect of cowling on cylinder temperatures and performance of a Wright J-5 engine, by Oscar W. Schey and Arnold E. Biermann, p. 635 , Technical Report No. 333. Full-scale turning characteristics of the U.S.S. Los Angeles, by F.L. Thompson, p. 657 , Technical Report No. 334. The torsion of members having sections common in aircraft construction, by George W. Trayer and H.W. March, p. 671 , Technical Report No. 335. Aerodynamic theory and test of strut forms II, by R.H. Smith, p. 721 , Technical Report No. 336. Tests of large airfoils in the propeller research tunnel, including two with corrugated surfaces, by Donald H. Wood, p. 761 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)