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 abstract in Soc Automotive Engrs -- J v 64 n 9 Aug 1956 p 25-7)


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    Titel :

    Stability and control of piloted aircraft at high altitudes


    Weitere Titelangaben:

    Soc Automotive Engrs -- Paper


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

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1955 Supersonic speeds



    Erscheinungsdatum :

    1955


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Stability and control of piloted aircraft at high altitudes

    Heald, E.R. | Engineering Index Backfile | 1956


    STABILITY AND CONTROL OF PILOTED AIRCRAFT AT HIGH ALTITUDES

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


    REMOTELY PILOTED AIRCRAFT

    RICCI JACOPO | Europäisches Patentamt | 2016

    Freier Zugriff

    Design aims for stability and control of piloted aircraft

    NATO, Fluid Dynamics Panel | SLUB | 1961


    Design aims for stability and control of piloted aircraft

    Allwright, H.J. | Engineering Index Backfile | 1961