THIS paper tells how to obtain and evaluate maximum speed of airplanes in level flight.Relationship between available thrust horsepower and powers required to overcome both induced and non-induced resistances is given, in order to provide a clearer understanding of the items affecting maximum speed and the various ways of evaluating changes in that speed.Maintenance of a constant density altitude in combination with a constant engine power or airplane speed is most satisfactory, the authors show.Charts enabling a pilot to attain these conditions in flight are given, together with a method of manifold-pressure calibration of the engine and the use of such calibration in determining the engine power in flight.


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    Titel :

    Airplane Flight Testing for Maximum Speed


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Thomas, F. M. (Autor:in) / Fairchild, H. W. (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    01.01.1933




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Airplane flight testing for maximum speed

    Thomas, F.M. / Fairchild, H.W. | Engineering Index Backfile | 1933


    Airplane Configurations for High-Speed Flight

    Johnson, Clarence L. | SAE Technical Papers | 1954


    Airplane configurations for high speed flight

    Johnson, C.L. | Engineering Index Backfile | 1953


    Airplane configurations for high speed flight

    Johnson, C.L. | Engineering Index Backfile | 1954


    Airplane configurations for high speed flight

    Johnson, C.L. | Engineering Index Backfile | 1953