Cite
Numerical study of unsteady flow and cooling characteristics of turbine blade cutback trailing edges integrated with pin fins and film holes.
MLA
Li, Yuefeng, et al. “Numerical Study of Unsteady Flow and Cooling Characteristics of Turbine Blade Cutback Trailing Edges Integrated with Pin Fins and Film Holes.” Aerospace Science & Technology, vol. 126, July 2022, p. N.PAG. EBSCOhost, https://doi.org/10.1016/j.ast.2022.107604.
APA
Li, Y., Xu, H., Wang, J., Zhu, J., & Su, H. (2022). Numerical study of unsteady flow and cooling characteristics of turbine blade cutback trailing edges integrated with pin fins and film holes. Aerospace Science & Technology, 126, N.PAG. https://doi.org/10.1016/j.ast.2022.107604
Chicago
Li, Yuefeng, Huazhao Xu, Jianhua Wang, Junqiang Zhu, and Hang Su. 2022. “Numerical Study of Unsteady Flow and Cooling Characteristics of Turbine Blade Cutback Trailing Edges Integrated with Pin Fins and Film Holes.” Aerospace Science & Technology 126 (July): N.PAG. doi:10.1016/j.ast.2022.107604.