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 (717 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. 8161

Note: A study of airplane maneuvers with special reference to angular velocities, by H.J.E. Reid [No. 155], p. 561 , A study of taking off and landing an airplane, by T. Carroll [No. 154], p. 553 , Analysis of stresses in German airplanes, by Wilhelm Hoff [No. 143], p. 263 , Controllability and maneuverability of airplanes, by F.H. Norton and W.G. Brown [No. 153], p. 535 , Damping coefficients due to tail surfaces in aircraft, by Lynn Chu [No. 136], p. 111 , Experimental research on air propellers, V, by W.F. Durand and E.P. Lesley [No. 141], p. 167 , General biplane theory, by Max M. Munk [No. 151], p. 473 , General theory of thin wing sections, by Max M. Munk [No. 142], p. 243 , Influence of model surface and air flow texture on resistance of aerodynamic bodies, by A.F. Zahm [No. 139], p. 151 , Internal stresses in laminated construction, by Forest Products Laboratory [No. 145], p. 325 , Lift and drag effects of wing-tip rake, by A.F. Zahm, R.M. Bear, and G.C. Hill [No. 140], p. 157 , List of technical reports, p. VIII , Mathematical equations for heat conduction in the fins of air-cooled engines, by D.R. Harper and W.B. Brown [No. 158], p. 677 , Nomenclature for aeronautics, by National Advisory Committee for Aeronautics [No. 157], p. 617 , Performance of B.M.W. 185-horsepower airplane engine, by S.W. Sparrow [No. 135], p. 101 , Performance of Maybach 300-horsepower airplane engine, by S.W. Sparrow [No. 134], p. 89 , Point drag and total drag of Navy struts no. 1 modified, by A.F. Zahm, R.H. Smith, and G.C. Hill [No. 137], p. 125 , Pressure distribution over the rudder and fin of an airplane in flight, by F.H. Norton and W.G. Brown [No. 149], p. 439 , Pressure distribution over thick airfoils -- model tests, by F.H. Norton and D.L. Bacon [No. 150], p. 449 , Standard atmosphere, by W.R. Gregg [No. 147], p. 397 , Table of contents, p. VII , The aerodynamic properties of thick airfoils, II, by F.H. Norton and D.L. Bacon [No. 152], p. 519 , The altitude effect on air speed indicators, II, by H.N. Eaton and W.A. MacNair [No. 156], p. 571 , The decay of a simple eddy, by H. Bateman [No. 144], p. 317 , The drag of 'C' class airship hull with varying length of cylindric midships, by A. F. Zahm, R.H. Smith, and G.C. Hill [No. 138], p. 141 , The pressure distribution over the horizontal tail surfaces of an airplane, III, by F.H. Norton and W. G. Brown [No. 148], p. 411 , The six-component wind balance, by A.F. Zahm [No. 146], p. 383 , The tail plane, by Max M. Monk [No. 133], p. 53 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

UID:

Format: Online-Ressource (519 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. 8873

Note: Appendix, p. 218 , Table of contents, p. VI , Technical Report No. 257. Pressure distribution over a wing and tail rib of a VE-7 and of a TS airplane in flight, by J.W. Crowley, Jr., p. 77 , Technical Report No. 258. Some factors affecting the reproducibility of penetration and the cut-off of oil sprays for fuel injected engines, by E.G. Beardsley, p. 115 , Technical Report No. 259. Characteristics of propeller sections tested in the variable density wind tunnel, by Eastman N. Jacobs, p. 125 , Technical Report No. 260. The effect of a flap and ailerons on the N.A.C.A. M-6 airfoil section, by George J. Higgins and Eastman N. Jacobs, p. 141 , Technical Report No. 261. Resistance and cooling power of various radiators, by R.H. Smith, p. 161 , Technical Report No. 262. Friction of aviation engines, by S.W. Sparrow and M.A. Thorne, p. 177 , Technical Report No. 263. Preliminary flight tests of the N.A.C.A. Roots type aircraft engine supercharger, by Arthur W. Gardiner and Elliott G. Reid, p. 205 , Technical Report No. 264. Differential pressures on a pilot-venturi and a pilot-static nozzle over 360 degree pitch and yaw, by R.M. Bear, p. 221 , Technical Report No. 265. A full scale investigation of ground effect, by Elliott G. Reid, p. 231 , Technical Report No. 266. Air force and moment for N-20 wing with certain cut-outs, by R.H. Smith, p. 239 , Technical Report No. 267. Drag of wings with end plates, by Paul E. Henke, p. 251 , Technical Report No. 268. Factors in the design of centrifugal type injection valves for oil engines, by W.F. Joachim and E.G. Beardsley, p. 265 , Technical Report No. 269. Air force tests of Sperry Messenger model with six sets of wings, by James M. Shoemaker, p. 281 , Technical Report No. 270. The measurement of pressure through tubes in pressure distribution tests, by Paul E. Henke, p. 301 , Technical Report No. 271. Pressure distribution tests on PW-9 wing models, showing effects of biplane interference, by A.J. Fairbanks, p. 313 , Technical Report No. 272. The relative performance obtained with several methods of control of an overcompressed engine using gasoline, by Arthur W. Gardiner and William E. Whedon, p. 327 , Technical Report No. 273. Wind tunnel tests on autorotation and the "flat spin," by Montgomery Knight, p. 341 , Technical Report No. 274. The N.A.C.A. photographic apparatus for studying fuel sprays from oil injection valves and test results from several researches, by Edward G. Beardsley, p. 359 , Technical Report No. 275. The effect of the walls in closed type wind tunnels, by George J. Higgins, p. 373 , Technical Report No. 276. Combustion time in the engine cylinder and its effect on engine performance, by Charles F. Marvin, Jr., p. 391 , Technical Report No. 277. The comparative performance of an aviation engine at normal and high inlet air temperatures, by Arthur W. Gardiner and Oscar W. Schey, p. 407 , Technical Report No. 278. Lift, drag, and elevator hinge moments of Handley Page control surfaces, by R.H. Smith, p. 427 , Technical Report No. 279. Tests on models of three British airplanes in the variable density wind tunnel, by George J. Higgins and George L. DeFoe, p. 449 , Technical Report No. 280. The gaseous explosive reaction -- the effect of inert gases, by F.W. Stevens, p. 477 , Technical Report No. 281. The effects of fuel and cylinder gas densities on the characteristics of fuel sprays for oil engines, by W.F. Joachim and Edward G. Beardsley, p. 489 , Technical Report No. 282. The performance of several combustion chambers designed for aircraft oil engines, by William F. Joachim and Carlton Kemper, p. 499 , © 2007 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)