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

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Опубликовано в::	Aerospace vol. 12, no. 12 (2025), p. 1063-1088
Главный автор:	Chen, Zheng
Другие авторы:	Ai Xinyu, Feng Weizhe, Yang, Rui, Qian, Wei
Опубликовано:	MDPI AG
Предметы:	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
Online-ссылка:	Citation/Abstract Full Text + Graphics Full Text - PDF
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