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

Spremljeno u:

Bibliografski detalji
Izdano u:	Aerospace vol. 12, no. 12 (2025), p. 1063-1088
Glavni autor:	Chen, Zheng
Daljnji autori:	Ai Xinyu, Feng Weizhe, Yang, Rui, Qian, Wei
Izdano:	MDPI AG
Teme:	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 pristup:	Citation/Abstract Full Text + Graphics Full Text - PDF
Oznake:	Dodaj oznaku Bez oznaka, Budi prvi tko označuje ovaj zapis!

Budi prvi tko komentira!