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    Methods used in NACA tank for investigation of longitudinal stability characteristics of models of flying boats

    Olson, R.E. / Land, N.S. | Engineering Index Backfile | 1643
    Investigation of suitable methods for evaluating stability and determining design parameters which have important effect on porpoising ...
    Publisher: National Advisory Committee for Aeronautics

    Report of the U. S. National advisory committee for aeronautics

    Engineering Index Backfile | 1919
    Activities of Committee between Oct. 4, 1917, and Oct. 10, 1918. ...

    National advisory committee report

    Engineering Index Backfile | 1919
    Recommendations regarding future development of American aeronautics; power plants for aircraft; materials for aircraft. ...

    Nomenclature for aeronautics

    Engineering Index Backfile | 1919
    From reports issued by Nat. Advisory Committee for Aeronautics. ...
    Keywords: Aeronautics

    Model test on fairing for chassis axle

    Griffiths, E. A. / Powell, C. H. | SLUB | 1919

    Apparatus for the measurements of M q on a complete model aeroplane

    Bryant, L. W. / Irving, H. B. | SLUB | 1919

    Notes on the design of a recording three-dimensional accelerometer for use in aeroplanes

    Searle, G. F. C. | SLUB | 1919

    The design of wind tunnels and wind tunnel propellers

    Warner, Edward P. / Norton, F.H. / Hebbert, C.M. | Engineering Index Backfile | 1919
    Publisher: National Advisory Committee for Aeronautics

    The strength of one-piece solid, built-up and laminated wood aeroplane wing beams

    Nelson, John H. | Engineering Index Backfile | 1919
    Tests conducted at Bureau of Standards to determine suitability of common wood as substitute for spruce. (See also in Aerial Age, vol. 10 ...
    Publisher: National Advisory Committee for Aeronautics

    An investigation of the aerodynamic properties of wing ailerons

    The effect of variation of chord of aileron. The effect of "wash-out" on ailerons [u.a.] / by H. B. Irving, and E. Ower
    Irving, H. B. / Ower, Ernest | SLUB | 1919

    Distribution of pressure over the tailplane of a De H.4 aeroplane

    Royal Aircraft Establishment, Aerodynamics Staff | SLUB | 1919

    Summery of present state of knowledge with regard to airscrews

    MacKinnon Wood, R. | SLUB | 1919

    Investigation on the efficiency of reverse rotating propellers in tandem

    Lanchester, Frederick W. | SLUB | 1919

    The variation of engine power with height

    Pinsent, D. H. / Renwick, H. A. | SLUB | 1919

    Heat transmission over surfaces

    Stanton, T. E. / Pannell, John Robert / Marshall, Dorothy | SLUB | 1919

    Forces and moments on a model of S.E.5 yawed, rolled and pitched, in accordance with the instructions given in a letter from controller, Technical Department, September 14th, 1918, REF. 52659-APT

    Bryant, L. W. | SLUB | 1919

    A comparison between two model aeroplanes differing only in plan form of wings and the corresponding full-scale aeroplanes

    Royal Aircraft Establishment, Wind Channel Staff | SLUB | 1919

    The bending, vibrating and whirling of loaded shafts

    Morris, Joseph | SLUB | 1919

    The approximate solution of linear differential equations

    Griffith, A. A. | SLUB | 1919

    Supplies and production of aircraft woods

    Engineering Index Backfile | 1919
    Publisher: National Advisory Committee for Aeronautics

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