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

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Opis bibliograficzny
Wydane w:	Aerospace vol. 12, no. 12 (2025), p. 1063-1088
1. autor:	Chen, Zheng
Kolejni autorzy:	Ai Xinyu, Feng Weizhe, Yang, Rui, Qian, Wei
Wydane:	MDPI AG
Hasła przedmiotowe:	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
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