Low-speed aerodynamics of aircraft shapes suitable for supersonic speeds; wind tunnel tests on model with boundary layer control methods applied; work aimed at clarifying requirements for handling qualities of future aircraft; flight tests on Avro 707A aircraft, with artificially worsened characteristics show that substantially constant performance in piloting task can be achieved at expense of increased pilot effort; conclusions on desirable levels of speed stability and phugoid damping drawn.


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    Title :

    Some low-speed problems of high-speed aircraft


    Additional title:

    AGARD -- Report


    Contributors:
    Spence, A. (author) / Lean, D. (author)

    Published in:

    Publication date :

    1961


    Size :

    38 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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