Research on Optimum Design of Composite Plate Wings for Aeroelastic Characteristics Using Lamination Parameters (The Second Report)-Optimum Design of Composite Plate Wings for Flutter and Divergence Characteristics-
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
doi 10.2322/jjsass.51.449
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Date
January 1, 2003
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Japan Society for Aeronautical and Space Sciences