Behavior of hydraulic flight-control systems exposed to high temperatures encountered by supersonic aircraft and effect on systems stability; temperature-response (T-R) diagram makes it possible to analyze such temperature effects; it contains rectangular locus of safe operating conditions, and may be used for determination of mechanical or thermal system equalizers which neutralize adverse temperature influences; principle of T-R diagram.


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    Titel :

    Temperature-response diagram


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Lermer, A.S. (Autor:in)

    Kongress:

    SAE Meeting ; 1961 Control equipment



    Erscheinungsdatum :

    1961


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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