An Experimental and CFD Investigation of a Supersonic Nonisobaric Jet Exhausting From a Beveled Nozzle
Keyword(s):
The aim of the investigation is to understand the shock-wave structure of the supersonic jet exhausting from a beveled nozzle. Results of investigation are presented as cross section Pitotpressure fields. This data can be used for verification of CFD results. The experiment was complemented by numerical simulation with using of the program packet ANSYS Fluent. The satisfactory qualitative agreement was obtained
1974 ◽
Vol 14
(9)
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pp. 873-886
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2009 ◽
Vol 26
(1)
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pp. 1-8
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1998 ◽
Vol 64
(619)
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pp. 732-739
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1974 ◽
Vol 14
(12)
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pp. 1303-1315
2021 ◽
Vol 1959
(1)
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pp. 012032