41–60 of 2,113 hits
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    Analysis of W. F. Durand's and E.P. Lesley's propeller tests

    Munk, Max M. | Engineering Index Backfile | 1923
    Publisher: National Advisory Committee for Aeronautics

    The vertical, longitudinal, and lateral accelerations experienced by an S. E. 5A airplane while maneuvering

    Norton, F.H. / Carroll, T. | Engineering Index Backfile | 1923
    Publisher: National Advisory Committee for Aeronautics

    The measurement of the damping in roll on a JN4th in flight

    Norton, F.H. | Engineering Index Backfile | 1923
    Investigation carried out for measuring value of Lp in flight; results show that damping found in wind tunnel by method of small ...
    Publisher: National Advisory Committee for Aeronautics

    Compressive strength of tapered airplane struts

    Lewe, Viktor | Engineering Index Backfile | 1923
    Methods for ascertaining value of n in Euler's simplified formula for compressive strength of tapered airplane struts, by estimating from ...
    Publisher: National Advisory Committee for Aeronautics

    Tests on built-up airplane struts having initial tension in outside fibers

    Schwamb, T.A. / Smith, C.S. | Engineering Index Backfile | 1923
    Abstract of a thesis prepared by authors in June 1922, as required for degree of Bachelor of Science at Mass. Inst. of Technology. (14 Figs ...
    Publisher: National Advisory Committee for Aeronautics

    Downwash of airplane wings

    Munk, Max / Cairo, Gunther | Engineering Index Backfile | 1923
    Publisher: National Advisory Committee for Aeronautics

    Flight characteristics

    Engineering Index Backfile | 1923
    Publisher: National Advisory Committee for Aeronautics

    Determination of climbing ability

    Blasius, H. | Engineering Index Backfile | 1923
    Publisher: National Advisory Committee for Aeronautics

    Thrust and power required in climbing, Georg Koenig

    Engineering Index Backfile | 1923
    It is shown that phenomena of climbing flight can be determined with sufficient accuracy, and represented very clearly, for all flight ...
    Publisher: National Advisory Committee for Aeronautics

    General theory of stresses in rigid airship, ZR-1

    Watters Pagon, W. | Engineering Index Backfile | 1923
    Publisher: National Advisory Committee for Aeronautics

    Experiments with a built-in or fuselage radiator

    Wieselsberger, C. | Engineering Index Backfile | 1923
    Publisher: National Advisory Committee for Aeronautics

    The air propeller, its strength and correct shape

    Dietsius, H. | Engineering Index Backfile | 1923
    Publisher: National Advisory Committee for Aeronautics

    Reduction in efficiency of propellers due to slipstream

    Munk, Max M. | Engineering Index Backfile | 1923
    Publisher: National Advisory Committee for Aeronautics

    The flexible mounting of the airplane engine

    Kutzbach, K. | Engineering Index Backfile | 1923
    Publisher: National Advisory Committee for Aeronautics

    The fairing of airfoil contours

    Warner, Edward P. | Engineering Index Backfile | 1923
    Publisher: National Advisory Committee for Aeronautics

    Practical method for balancing airplane moments

    Hamburger, H. | Engineering Index Backfile | 1924
    Publisher: National Advisory Committee for Aeronautics

    The application of propeller test data to design and performance calculations

    Diehl, W.S. | Engineering Index Backfile | 1924
    Publisher: National Advisory Committee for Aeronautics

    A new relation between the induced yawing moment and the rolling moment of an airfoil in straight motion

    Munk, M.M. | Engineering Index Backfile | 1924
    Publisher: National Advisory Committee for Aeronautics

    Elements of the wing section theory and of the wing theory

    Munk, M.M. | Engineering Index Backfile | 1924
    Publisher: National Advisory Committee for Aeronautics