Analysis of Supersonic Free Jets and Impinging Supersonic Jets on Deflector

<p id="p1">The computational fluid dynamics analysis is carried out to analyze the shock and flow characteristics of under- and over expanded supersonic free jets emanating from convergent-divergent nozzles. Influence of exit Mach number on shock cell lengths are analyzed with the help of density co...

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Detalles Bibliográficos

Autor principal:	Mehta, Rakhab
Formato:	Capítulo de libro
Lenguaje:	inglés
Publicado:	IntechOpen 2023
Materias:	Physical Sciences, Engineering and Technology
Acceso en línea:	https://www.intechopen.com/chapters/1158370
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