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pro vyhledávání: '"Eun-Soo Go"'
Publikováno v:
Shock and Vibration, Vol 2018 (2018)
The panel structures of flight vehicles at supersonic or hypersonic speeds are subjected to combined thermal, acoustic, and aerodynamic loads. Because of the combined thermal and acoustic loads, the panel structure may exhibit nonlinear random vibrat
Externí odkaz:
https://doaj.org/article/f4f916ebdc6b410baa04fdfef7cf4ebd
Publikováno v:
Shock and Vibration, Vol 2018 (2018)
The panel structures of flight vehicles at supersonic or hypersonic speeds are subjected to combined thermal, acoustic, and aerodynamic loads. Because of the combined thermal and acoustic loads, the panel structure may exhibit nonlinear random vibrat