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Publications by Hideki Sekine
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
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Aeroelastic Analysis of Composite Wings
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An Aeroelastic Metamodel Based on Experimental Data for Flutter Prediction of Swept Rectangular Wings
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Optimum Design of LCL Filter Parameters for Photovoltaic Inverters
Optimum Design of Fibrous Laminated Composite Plates Subject to Biaxial Compression.
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Flutter of Aeroplane Wings.
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Elastic Buckling Characteristics and Optimum Rigidity of Stiffened Plate Under Bending and Shear Stress
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