APA (7e ed.) Bronvermelding
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
Chicago (17e ed.) Bronvermelding
Chen, Zheng, Ai Xinyu, Feng Weizhe, Rui Yang, en 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.
MLA (9e ed.) Bronvermelding
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.
Let op: Deze citaties zijn niet altijd 100% accuraat.