The results that are described in this article form a complete series of tests on an airfoil fitted with front and rear slots, the rear slot being formed between the portion of the wing aft of the rear spar and the forward portion of the flap.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Tests on an Airfoil with Two Slots Suitable for an Aircraft of High Performance : Lift, Drag, Rolling and Yawing Moment Measurements


    Contributors:

    Publication date :

    1926-07-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Analysis of Lift Force, Drag Force, Side Force, Pitching Moment, Yawing Moment, and Rolling Moment

    Sinkovec, Bryan / Loshek, Patrick / Mendes Alves, Rodrigo et al. | AIAA | 2015


    Analysis of Lift Force, Drag Force, Side Force, Pitching Moment, Yawing Moment, and Rolling Moment (AIAA 2015-1888)

    Amano, Ryoichi S. / Yen, Yi-Hsin / Sinkovec, Bryan et al. | British Library Conference Proceedings | 2015


    Aircraft spin characteristics with high-alpha yawing moment asymmetry

    Malik, Bilal / Akhtar, Suhail / Masud, Jehanzeb | SAGE Publications | 2018