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Cited 2 time in webofscience Cited 2 time in scopus
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On the RR -> MR transition of asymmetric shock waves in steady flows

Authors
Hu, Z. M.Kim, M. S.Myong, R. S.Cho, T. H.
Issue Date
Oct-2008
Publisher
SPRINGER
Keywords
regular reflection; Mach reflection; transition; asymmetric; shock waves
Citation
SHOCK WAVES, v.18, no.5, pp 419 - 423
Pages
5
Indexed
SCIE
SCOPUS
Journal Title
SHOCK WAVES
Volume
18
Number
5
Start Page
419
End Page
423
URI
https://scholarworks.gnu.ac.kr/handle/sw.gnu/27261
DOI
10.1007/s00193-008-0164-8
ISSN
0938-1287
1432-2153
Abstract
In this paper, RR -> MR transition of asymmetric shock waves has been theoretically studied. The transition can occur between the sonic-point and maximum-deflection criteria due to the the effects of expansion fans which are inherent flow structures. Comparison shows a better agreement among experiments and the analytical results. Some discrepancies reported in previous studies among experiments and theory have also been explained based on the threshold for RR -> MR transition.
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Myong, Rho Shin
대학원 (기계항공우주공학부)
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