Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    AIAA-2001-1205 Composite Wing Structural Design Optimization with Continuity Constraints



    Conference:

    42nd, Structures, structural dynamics, and materials conference ; 2001 ; Seattle, WA



    Publication date :

    2001-01-01


    Size :

    12 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Preliminary Wing Weight Estimation Under Probabilistic Loads for a Transport Aircraft (AIAA 2014-1205)

    Corman, J.A. / Rancourt, D. / Lee, C. et al. | British Library Conference Proceedings | 2014


    AIAA 2006-1205 A Coupled Approach for Plasma-Based Flow Control Simulations of Wing Sections

    Gaitonde, D. V. / Visbal, M. R. / Roy, S. et al. | British Library Conference Proceedings | 2006


    Nr. 1205

    DataCite | 1868

    Free access

    1205-1235 An Application of Numerical Optimization to a Wing Twist of SST Wing-Nacelle Configuration

    Yamazaki, T. / Saito, M. / National Aerospace Technology | British Library Conference Proceedings | 2000