Design and Optimization Method for Scaled Equivalent Model of T-Tail Configuration Structural Dynamics Simulating Fuselage Stiffness

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書誌詳細
出版年:	Aerospace vol. 12, no. 12 (2025), p. 1063-1088
第一著者:	Chen, Zheng
その他の著者:	Ai Xinyu, Feng Weizhe, Yang, Rui, Qian, Wei
出版事項:	MDPI AG
主題:	Finite element method Aircraft aerodynamics Software Fuselages Optimization techniques Wind tunnel testing Equivalence Transport aircraft Least squares method Flutter Wind tunnels Multiple objective analysis Dynamic characteristics Modal assurance criterion Design Airframes Aircraft Flight safety Simulation Aircraft structures Upper bounds Confidence intervals Aerodynamics Objective function Wind tunnel models Mathematical models Errors Algorithms Design optimization Vibration tests
オンライン･アクセス:	Citation/Abstract Full Text + Graphics Full Text - PDF
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