It is shown that when secondary effects are neglected, maximum available increase in lift due to power is equal to thrust being developed; if increase in lift due to power is expressed in coefficient form, very high values may be shown under conditions which are found to be wholly impracticable in flight.


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    Titel :

    Some fundamental considerations in regard to use of power in landing airplane


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Diehl, W.S. (Autor:in)


    Erscheinungsdatum :

    1939


    Format / Umfang :

    7 pages


    Anmerkungen:

    3 Supp sheets, Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :