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.
Performance Improvement of Composite Wings through Aeroelastic Tailoring and Modern Control
1995
110 pages
Report
Keine Angabe
Englisch
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