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Coupled Flow-Thermal Analysis of a Rocket Nozzle with Charring Ablative Thermal Protection System

Fuente: arXiv

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Detalles Bibliográficos
Autores principales:	Sheikh, Basit G., Kumar, Rakesh, S, Susheel Kumar
Formato:	Preprint
Publicado:	2024
Materias:	Fluid Dynamics
Acceso en línea:	Acceder al recurso
Etiquetas:	Agregar Etiqueta Sin Etiquetas, Sea el primero en etiquetar este registro!

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