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
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Chicago Style (17th ed.) Zitazioa
Chen, Zheng, Ai Xinyu, Feng Weizhe, Rui Yang, eta 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.
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MLA (9th ed.) Zitazioa
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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