Enhancement of Film Cooling Effectiveness in a Supersonic Nozzle

Film cooling as applied to rocket nozzles is analyzed numerically with emphasis on the assessment of the effect of the mixing of coolant with the hot stream. Cooling performance, as characterized by cooling effectiveness, is studied for three different coolants in the three-dimensional, turbulent fl...

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Autors principals:	Nithin Somasekharan, A. R. Srikrishnan, Harihara Sudhan Kumar, Krishna Prasad Ganesh, Akram Mohammad, Ratna Kishore Velamati
Format:	Artigo
Idioma:	Inglês
Publicat:	MDPI AG 2023-03-01
Col·lecció:	Entropy
Matèries:	rocket nozzle cooling mixing layer studies diffuser-type coolant injector film cooling
Accés en línia:	https://www.mdpi.com/1099-4300/25/3/481
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