Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Stability derivatives for a delta-wing X-31 aircraft validated using wind tunnel test data


    Contributors:


    Publication date :

    2011



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.60 Raumfahrttechnik
    Local classification TIB:    275/7040



    Stability derivatives for a delta-wing X-31 aircraft validated using wind tunnel test data

    Anton, N / Botez, R M / Popescu, D | SAGE Publications | 2011


    Wind Tunnel Test of a Very Flexible Aircraft Wing

    Britt, Robert / Ortega, Daniel / Mc Tigue, John et al. | AIAA | 2012


    Wind Tunnel Test of a Very Flexible Aircraft Wing

    Britt, R. / Ortega, D. / McTigue, J. et al. | British Library Conference Proceedings | 2012


    Adaptive Control of Slender Delta Wing Rock in Stability Wind Tunnel

    Vaidya, Sachidanand D. | Online Contents | 1997


    WIND TUNNEL TEST RESULTS FOR A CANARD ROTOR/WING AIRCRAFT CONFIGURATION

    Thompson, T. L. / Smith, R. L. / Helwani, M. et al. | British Library Conference Proceedings | 2001