Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Optimization Procedure with Analytical Aerodynamic Sensitivity for Reduced Sonic Boom Design



    Published in:

    Publication date :

    1996



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.50
    Local classification TIB:    770/7040



    Optimization procedure with analytical aerodynamic sensitivity for reduced sonic boom design

    Pagaldipti, N. S. / Rajadas, J. N. / Chattopadhyay, A. | AIAA | 1996


    Optimization procedure for reduced sonic boom in high speed flight

    Chattopadhyay, A / Narayan, J / Pagaldipti, N et al. | AIAA | 1995


    HSCT design for reduced sonic boom

    Haglund, George T. | NTRS | 1992


    Aerodynamic Design of Shaped Sonic Boom Demonstration Aircraft

    Graham, David / Dahlin, John / Meredith, Keith et al. | AIAA | 2005


    Aerodynamic Design of Shaped Sonic Boom Demonstration Aircraft

    Graham, D. H. / Dahlin, J. A. / Meredith, K. B. et al. | British Library Conference Proceedings | 2005