The results of computational studies of the gas-dynamic and geometric parameters of supersonic gas jets outflowing from axisymmetric nozzles into a submerged space with strong underexpansion are presented based on the finite volume method and the marching method.
Outflow of Supersonic Gas Jets from Axisymmetric Nozzle into a Space with a High Nozzle Pressure Ratios
Russ. Aeronaut.
Russian Aeronautics ; 66 , 2 ; 232-241
01.04.2023
10 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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