Investigation consisted of force tests of model and wing alone for angle of attack range from -- 8 to 12° and for momentum coefficients up to about 3.0; results indicated that double slotted flap arrangement was more efficient in terms of lift and drag than external flow single slotted flap arrangements previously tested.


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    Titel :

    Wind-tunnel investigation of small-scale sweptback-wing jet-transport model equipped with external-flow jet-augmented double slotted flap


    Weitere Titelangaben:

    NASA Memo


    Beteiligte:


    Erscheinungsdatum :

    1959


    Format / Umfang :

    41 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :