Effects of Feeding Mach Numbers on the Flowfield Structures of Supersonic Film Cooling

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Effects of Feeding Mach Numbers on the Flowfield Structures of Supersonic Film Cooling

Effects of Feeding Mach Numbers on the Flowfield Structures of Supersonic Film Cooling

Song, Changqing / Shen, Chibing

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Title :

Effects of Feeding Mach Numbers on the Flowfield Structures of Supersonic Film Cooling

Contributors:

Song, Changqing (author) / Shen, Chibing (author)

Published in:

Journal of Thermophysics and Heat Transfer ; 33 , 1 ; 264-270

Publication date :

2018-09-13

Size :

7 pages

ISSN :

0887-8722 , 1533-6808

DOI :

https://doi.org/10.2514/1.T5475

Type of media :

Article (Journal)

Type of material :

Electronic Resource

Language :

English

Keywords :

Mach Numbers , Film Cooling , Coolant , Boundary Layer Thickness , Laval Nozzle , Direct Numerical Simulation , Reynolds Averaged Navier Stokes , Shock Wave Generators , Rocket Engine , Mass Flow Rate

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