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    Title :

    Aeronautics. Thirteenth annual report of the National Advisory Committee for Aeronautics, 1927




    Publication date :

    1928


    Size :

    Online-Ressource (519 p)


    Remarks:

    illustrations, tables
    Campusweiter Zugriff (Universität Hannover) - Vervielfältigungen (z.B. Kopien, Downloads) sind nur von einzelnen Kapiteln oder Seiten und nur zum eigenen wissenschaftlichen Gebrauch erlaubt. Keine Weitergabe an Dritte. Kein systematisches Downloaden durch Robots.
    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
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    Type of media :

    Book


    Type of material :

    Electronic Resource


    Language :

    English