The research has been carried out simultaneously on three aspects of aircraft wings performance optimization, as follows: (1) Structural tailoring and modern control of thin-walled model of composite aircraft wings; (2) Structural tailoring of a low-aspect ratio plate model of composite aircraft wings; and (3) Integrated structural design and vibration control by multiobjective optimization. Significant progress has been made on all fronts.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Performance Improvement of Composite Wings through Aeroelastic Tailoring and Modern Control


    Contributors:

    Publication date :

    1995


    Size :

    110 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







    Active Aeroelastic Tailoring of High Aspect Ratio Composite Wings

    Cesnik, C. E. S. / Ortega Morales, M. / Patil, M. et al. | British Library Conference Proceedings | 2000


    Active aeroelastic tailoring of high aspect ratio composite wings

    Cesnik, Carlos / Ortega-Morales, Miguel / Patil, Mayuresh | AIAA | 2000