Cite
Experimental investigations of the effects of the injection angle and blowing ratio on the leading-edge film cooling of a rotating twisted turbine blade.
MLA
Li, Hai-wang, et al. “Experimental Investigations of the Effects of the Injection Angle and Blowing Ratio on the Leading-Edge Film Cooling of a Rotating Twisted Turbine Blade.” International Journal of Heat & Mass Transfer, vol. 127, Dec. 2018, pp. 856–69. EBSCOhost, https://doi.org/10.1016/j.ijheatmasstransfer.2018.07.133.
APA
Li, H., Han, F., Zhou, Z., Ma, Y., & Tao, Z. (2018). Experimental investigations of the effects of the injection angle and blowing ratio on the leading-edge film cooling of a rotating twisted turbine blade. International Journal of Heat & Mass Transfer, 127, 856–869. https://doi.org/10.1016/j.ijheatmasstransfer.2018.07.133
Chicago
Li, Hai-wang, Feng Han, Zhi-yu Zhou, Yi-wen Ma, and Zhi Tao. 2018. “Experimental Investigations of the Effects of the Injection Angle and Blowing Ratio on the Leading-Edge Film Cooling of a Rotating Twisted Turbine Blade.” International Journal of Heat & Mass Transfer 127 (December): 856–69. doi:10.1016/j.ijheatmasstransfer.2018.07.133.