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Numerical simulation of the shock-wave starting of an inlet tested in an impulse wind tunnel with a throttled plenum chamber
Author(s) -
Yu. P. Gounko,
N. I. Kavun
Publication year - 2021
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.177
H-Index - 75
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/5.0052059
Subject(s) - inlet , mechanics , plenum space , hypersonic wind tunnel , nozzle , wind tunnel , shock wave , oblique shock , supersonic wind tunnel , supersonic speed , engineering , geology , aerospace engineering , physics , mechanical engineering

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