Increasing altitude causes deterioration of important flight characteristics; aerodynamic damping suffers as ratio of true to indicated air speed increases; adequate static stability becomes more difficult under adverse influence of high supersonic speed and high angle of attack; all of these problems are amenable to solution; but they will not be forthcoming unless designers are prepared to accept new configurations. (See also Soc Automotive Engrs -- Paper n 603 for meeting Oct 11-15 1955 8 p)


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    Title :

    Stability and control of piloted aircraft at high altitudes


    Additional title:

    Soc Automotive Engrs -- J


    Contributors:
    Heald, E.R. (author)

    Published in:

    Publication date :

    1956


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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