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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    Titel :

    Stability and control of piloted aircraft at high altitudes


    Weitere Titelangaben:

    Soc Automotive Engrs -- J


    Beteiligte:
    Heald, E.R. (Autor:in)


    Erscheinungsdatum :

    1956


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Stability and control of piloted aircraft at high altitudes

    Heald, E.R. | Engineering Index Backfile | 1955


    STABILITY AND CONTROL OF PILOTED AIRCRAFT AT HIGH ALTITUDES

    HEALD, E. R. | SAE Technical Papers | 1955


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