Articles citing this article

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Cited article:

Effect of mainstream Mach number on the flow characteristics and cooling effectiveness of supersonic film cooling

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Numerical Heat Transfer, Part A: Applications 1 (2023)
https://doi.org/10.1080/10407782.2023.2287535

Comparison of Shock/Cooling-Film Interaction for Cooled and Isoenergetic Injection

Pascal Marquardt, Michael Klaas and Wolfgang Schröder
AIAA Journal 58 (5) 2078 (2020)
https://doi.org/10.2514/1.J058471

Experimental Investigation of Isoenergetic Film-Cooling Flows with Shock Interaction

Pascal Marquardt, Michael Klaas and Wolfgang Schröder
AIAA Journal 57 (9) 3910 (2019)
https://doi.org/10.2514/1.J058197

Effect of film cooling injection on aerodynamic performances of scramjet isolator

Kuan Zheng, Wei Tian, Jiang Qin, Silong Zhang and Hui Hu
Aerospace Science and Technology 105383 (2019)
https://doi.org/10.1016/j.ast.2019.105383