Design and principal advantages; high lift obtained without increasing total drag by using deep high-lift section for top wing and medium section for bottom wing; gives greater efficiency.


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    Title :

    "Gloster" high lift biplane wings


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Memorandum


    Contributors:


    Publication date :

    1927


    Size :

    5 pages


    Remarks:

    2 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    "Gloster" high lift biplane wings

    Preston, H E | NTRS | 1927


    Gloster. The "Gloster IV."

    Engineering Index Backfile | 1928


    Investigation of lift distribution over separate wings of biplane

    Kuechemann, D. | Engineering Index Backfile | 1939



    Convertible monoplane -- Biplane wings

    Hall, R.F. | Engineering Index Backfile | 1926