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

Gespeichert in:

Bibliographische Detailangaben
Veröffentlicht in:	Aerospace vol. 12, no. 12 (2025), p. 1063-1088
1. Verfasser:	Chen, Zheng
Weitere Verfasser:	Ai Xinyu, Feng Weizhe, Yang, Rui, Qian, Wei
Veröffentlicht:	MDPI AG
Schlagworte:	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-Zugang:	Citation/Abstract Full Text + Graphics Full Text - PDF
Tags:	Tag hinzufügen Keine Tags, Fügen Sie das erste Tag hinzu!

Schreiben Sie den ersten Kommentar!