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Cited article:
M. Konopka , M. Meinke , W. Schröder
Published online: 2013-06-14
This article has been cited by the following article(s):
6 articles
Effect of mainstream Mach number on the flow characteristics and cooling effectiveness of supersonic film cooling
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Large Eddy Simulation of Film Cooling: A Review
Joon Ahn Energies 15 (23) 8876 (2022) https://doi.org/10.3390/en15238876
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
Numerical Simulation of Shock Wave-Boundary Layer Interaction with Supersonic Film Cooling
Zhigang Liu IOP Conference Series: Earth and Environmental Science 526 (1) 012149 (2020) https://doi.org/10.1088/1755-1315/526/1/012149
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