Thermal-Aeroelastic Investigation of a Hypersonic Panel Vibration Based on a Developed MMC Method
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发表时间:2024-04-25
发表刊物:AEROSPACE
卷号:11
期号:3
关键字:FLUTTER; HARMONIC GRADIENT-METHOD; TOPOLOGY OPTIMIZATION
发表时间:2024-04-25
Thermal-Aeroelastic Investigation of a Hypersonic Panel Vibration Based on a Developed MMC Method
点击次数:
发表时间:2024-04-25
发表刊物:AEROSPACE
卷号:11
期号:3
关键字:FLUTTER; HARMONIC GRADIENT-METHOD; TOPOLOGY OPTIMIZATION
发表时间:2024-04-25