Wang, M.; Wang, Z.; Zhang, Y.; Cheng, D.; Tan, H.; Wang, K.; Gao, S.
Control of Cowl Shock/Boundary Layer Interaction in Supersonic Inlet Based on Dynamic Vortex Generator. Aerospace 2023, 10, 729.
https://doi.org/10.3390/aerospace10080729
AMA Style
Wang M, Wang Z, Zhang Y, Cheng D, Tan H, Wang K, Gao S.
Control of Cowl Shock/Boundary Layer Interaction in Supersonic Inlet Based on Dynamic Vortex Generator. Aerospace. 2023; 10(8):729.
https://doi.org/10.3390/aerospace10080729
Chicago/Turabian Style
Wang, Mengge, Ziyun Wang, Yue Zhang, Daishu Cheng, Huijun Tan, Kun Wang, and Simin Gao.
2023. "Control of Cowl Shock/Boundary Layer Interaction in Supersonic Inlet Based on Dynamic Vortex Generator" Aerospace 10, no. 8: 729.
https://doi.org/10.3390/aerospace10080729
APA Style
Wang, M., Wang, Z., Zhang, Y., Cheng, D., Tan, H., Wang, K., & Gao, S.
(2023). Control of Cowl Shock/Boundary Layer Interaction in Supersonic Inlet Based on Dynamic Vortex Generator. Aerospace, 10(8), 729.
https://doi.org/10.3390/aerospace10080729