On the RR→MR transition of asymmetric shock waves in steady flows |
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| Authors: | Z M Hu M S Kim R S Myong T H Cho |
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| Institution: | (1) Research Center for Aircraft Parts Technology, School of Mechanical and Aerospace Engineering, Gyeongsang National University, Jinju, 660-701, South Korea |
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| 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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| Keywords: | Regular reflection Mach reflection Transition Asymmetric Shock waves |
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