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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    Title :

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


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :