An Efficient Analysis Method of Aluminum Alloy Helicopter Fuselage Projectile Damage Based on Projectile Breakdown Theory.

MLA

Xing, Xiaobing, et al. “An Efficient Analysis Method of Aluminum Alloy Helicopter Fuselage Projectile Damage Based on Projectile Breakdown Theory.” Aerospace (MDPI Publishing), vol. 11, no. 6, June 2024, p. 500. EBSCOhost, https://doi.org/10.3390/aerospace11060500.

APA

Xing, X., Tan, J., Yang, Y., Yong, T., Yu, L., & Zhou, Y. (2024). An Efficient Analysis Method of Aluminum Alloy Helicopter Fuselage Projectile Damage Based on Projectile Breakdown Theory. Aerospace (MDPI Publishing), 11(6), 500. https://doi.org/10.3390/aerospace11060500

Chicago

Xing, Xiaobing, Jianfeng Tan, Yuxiao Yang, Tian Yong, Linjun Yu, and Yun Zhou. 2024. “An Efficient Analysis Method of Aluminum Alloy Helicopter Fuselage Projectile Damage Based on Projectile Breakdown Theory.” Aerospace (MDPI Publishing) 11 (6): 500. doi:10.3390/aerospace11060500.