Control of Cowl Shock/Boundary Layer Interaction in Supersonic Inlet Based on Dynamic Vortex Generator.

MLA

Wang, Mengge, et al. “Control of Cowl Shock/Boundary Layer Interaction in Supersonic Inlet Based on Dynamic Vortex Generator.” Aerospace (MDPI Publishing), vol. 10, no. 8, Aug. 2023, p. 729. EBSCOhost, https://doi.org/10.3390/aerospace10080729.

APA

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 (MDPI Publishing), 10(8), 729. https://doi.org/10.3390/aerospace10080729

Chicago

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 (MDPI Publishing) 10 (8): 729. doi:10.3390/aerospace10080729.