Results of study made with 45° swept-wing model; comparison with results for configuration with leading edge slats is included; devices provided only slight improvement of longitudinal stability characteristics but decreased aircraft drag coefficients at moderate and high lifting conditions.


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    Titel :

    Transonic investigation of aerodynamic characteristics of swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:


    Erscheinungsdatum :

    1961


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :