- Scholarly Journal
Design and Optimization Method for Scaled Equivalent Model of T-Tail Configuration Structural Dynamics Simulating Fuselage Stiffness
Design and Optimization Method for Scaled Equivalent Model of T-Tail Configuration Structural Dynamics Simulating Fuselage StiffnessChen, Zheng; Ai Xinyu; Feng Weizhe; Yang, Rui; Qian, Wei.
Aerospace; Basel Vol. 12, Iss. 12, (2025): 1063.
DOI:10.3390/aerospace12121063




