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    Wind-tunnel research comparing lateral control devices, particularly at high angles of attack

    Wind-tunnel research comparing lateral control devices, particularly at high angles of attack


    IV -- Floating Tip Ailerons on Rectangular Wings; general performance definitely poorer for all of rectangular wings with floating tip ailerons than with wing having same over-all dimensions and ordinary ailerons; at angles of attack above 22° control with wing-tip ailerons found to be greater than assumed satisfactory value.

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    Titel :

    Wind-tunnel research comparing lateral control devices, particularly at high angles of attack

    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report

    Beteiligte:
    Weick, F.E. (Autor:in) / Harris, T.A. (Autor:in) / Shortal, J.A. (Autor:in) / Noyes, R.W. (Autor:in) / Wenzinger, C.H. (Autor:in)
    Erschienen in:

    National Advisory Committee for Aeronautics -- Reports

    Erscheinungsdatum :

    1932

    Format / Umfang :

    25 pages

    Medientyp :

    Report

    Format :

    Print

    Sprache :

    Englisch

    Schlagwörter :

    Airplane control surfaces

    © Metadata Copyright Elsevier B. V. All rights reserved.

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