The effects of lift/drag ratio and gross-thrust/ram-drag ratio on the benefits to be obtained from thrust deflection are analyzed, and it is shown that combinations of low values of these parameters can result in a substantial advantage. For instance, at a lift/drag ratio of 4 and a gross-thrust/ram-drag ratio of 1.1, the range may be increased about 34 percent. The required increases in altitude and in engine capture area are also shown. (Author)


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    Titel :

    Thrust Deflection for Cruise


    Beteiligte:
    W. H. Krase (Autor:in)

    Erscheinungsdatum :

    1966


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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