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.


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    Titel :

    Performance Improvement of Composite Wings through Aeroelastic Tailoring and Modern Control


    Beteiligte:
    L. Meirovitch (Autor:in)

    Erscheinungsdatum :

    1995


    Format / Umfang :

    110 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    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