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

Tallennettuna:

Bibliografiset tiedot
Julkaisussa:	Aerospace vol. 12, no. 12 (2025), p. 1063-1088
Päätekijä:	Chen, Zheng
Muut tekijät:	Ai Xinyu, Feng Weizhe, Yang, Rui, Qian, Wei
Julkaistu:	MDPI AG
Aiheet:	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
Linkit:	Citation/Abstract Full Text + Graphics Full Text - PDF
Tagit:	Lisää tagi Ei tageja, Lisää ensimmäinen tagi!

Lisää ensimmäinen kommentti!