Li, X.; Lei, Q.; Zhao, X.; Fan, W.; Chen, S.; Chen, L.; Tian, Y.; Zhou, Q.
Combustion Characteristics of a Supersonic Combustor with a Large Cavity Length-to-Depth Ratio. Aerospace 2022, 9, 214.
https://doi.org/10.3390/aerospace9040214
AMA Style
Li X, Lei Q, Zhao X, Fan W, Chen S, Chen L, Tian Y, Zhou Q.
Combustion Characteristics of a Supersonic Combustor with a Large Cavity Length-to-Depth Ratio. Aerospace. 2022; 9(4):214.
https://doi.org/10.3390/aerospace9040214
Chicago/Turabian Style
Li, Xiang, Qingchun Lei, Xiaocun Zhao, Wei Fan, Shuang Chen, Li Chen, Ye Tian, and Quan Zhou.
2022. "Combustion Characteristics of a Supersonic Combustor with a Large Cavity Length-to-Depth Ratio" Aerospace 9, no. 4: 214.
https://doi.org/10.3390/aerospace9040214
APA Style
Li, X., Lei, Q., Zhao, X., Fan, W., Chen, S., Chen, L., Tian, Y., & Zhou, Q.
(2022). Combustion Characteristics of a Supersonic Combustor with a Large Cavity Length-to-Depth Ratio. Aerospace, 9(4), 214.
https://doi.org/10.3390/aerospace9040214