Cita APA (7a ed.)
Chen, Z., Xinyu, A., Weizhe, F., Yang, R., & Qian, W. (2025). Design and Optimization Method for Scaled Equivalent Model of T-Tail Configuration Structural Dynamics Simulating Fuselage Stiffness. Aerospace. https://doi.org/10.3390/aerospace12121063
Cita Chicago Style (17a ed.)
Chen, Zheng, Ai Xinyu, Feng Weizhe, Rui Yang, y Wei Qian. "Design and Optimization Method for Scaled Equivalent Model of T-Tail Configuration Structural Dynamics Simulating Fuselage Stiffness." Aerospace 2025. https://doi.org/10.3390/aerospace12121063.
Cita MLA (9a ed.)
Chen, Zheng, et al. "Design and Optimization Method for Scaled Equivalent Model of T-Tail Configuration Structural Dynamics Simulating Fuselage Stiffness." Aerospace, 2025, https://doi.org/10.3390/aerospace12121063.
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