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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Diehl, W.S. (author)


    Publication date :

    1939


    Size :

    7 pages


    Remarks:

    3 Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :