The up-to-date methods of computational fluid dynamics (CFD) were employed to study the effect of mass flux ratio above the submerged part of a solid rocket engine nozzle with a contoured inlet on the discharge coefficient. The results are given in correlation with the inlet geometry and nozzle submergence.
Effect of Mass Flux Ratio above the Submerged Part of a Nozzle with a Contoured Inlet on the Discharge Coefficient
Russ. Aeronaut.
Russian Aeronautics ; 63 , 2 ; 310-316
2020-04-01
7 pages
Article (Journal)
Electronic Resource
English
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