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    Title :

    Aeronautics. Twelfth annual report of the National Advisory Committee for aeronautics 1926




    Publication date :

    1927


    Size :

    Online-Ressource (640 p)


    Remarks:

    illustrations, maps, 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.
    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


    Type of media :

    Book


    Type of material :

    Electronic Resource


    Language :

    English