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

Wedi'i Gadw mewn:

Manylion Llyfryddiaeth
Cyhoeddwyd yn:	Aerospace vol. 12, no. 12 (2025), p. 1063-1088
Prif Awdur:	Chen, Zheng
Awduron Eraill:	Ai Xinyu, Feng Weizhe, Yang, Rui, Qian, Wei
Cyhoeddwyd:	MDPI AG
Pynciau:	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
Mynediad Ar-lein:	Citation/Abstract Full Text + Graphics Full Text - PDF
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