Xu Li-gong. The Interaction of a Shock Wave with the Boundary Layer in a Reflected Shock Tunnel[J]. Applied Mathematics and Mechanics, 1989, 10(6): 523-529.
Citation: Xu Li-gong. The Interaction of a Shock Wave with the Boundary Layer in a Reflected Shock Tunnel[J]. Applied Mathematics and Mechanics, 1989, 10(6): 523-529.

The Interaction of a Shock Wave with the Boundary Layer in a Reflected Shock Tunnel

  • Received Date: 1988-04-03
  • Publish Date: 1989-06-15
  • The influence of a nontotal reflection on the interaction of a reflected shock wave with the boundary layer in a reflected shock tunnel has been investigated. The calculating method of the velocity, the temperature and the Mach number profiles in the boundary layer in reflected shock fixed coordinates has been obtained. To account for equilibrium real gas effects of nitrogen, the numerical results show that the minimum Mach number in the boundary layer has been moved from the wall into the boundary layer with the increasing of the incident shock Mach number. The minimum Mach number, the shock angle in the bifurcated foot and the jet velocity along the wall to the end plate are reduced owing to the Increasing of the area of nozzle throat. The numerical results are in good agreement with measurements.
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  • [1]
    Mark,H.,The interaction of a reflected shock wave with the boundary layer in a shock tube,J.Aero.Sci.,24,April(1957),304-306.
    [2]
    Byron,S.and N.Rott,On the interaction of the reflected shock wave with the laminar boundary layer on the shock tube walls,Proceedings of the 1961 Heat Transfer and Fluid Mechanics Institute,Stanford Univ.Press(1961),38-54.
    [3]
    Davies,L.D.,The interaction of the reflected shock with the boundary layer in a shock tube and its influence on the duration of hot flow in the reflected shock tunnel,NPL Aero.Reports 1158 and 1167(1965).
    [4]
    Davies,L.D.and J.L.Wilson,Influence of reflected shock and boundary-layer interaction on shock tube flows,Physics of Fluids,12,Suppl.1(1969),37-43.
    [5]
    Matsuo,K.,K.Kage and S.Kawagoe,The interaction of a reflected shock wave with the contact region in a shock tube,Bulletin of the JSME,18,121,July(1975).
    [6]
    Stalker,R.J.and C.A.Crane,Driver gas contamination in a high enthalpy reflected shock tunnel,AIAA J.,16,3(1978),277-279.
    [7]
    Xu,L.G.and C.M.Gourlay,Reflected shock boundary layer interaction in a shock tube with boundary layer suction,Research Report No.14/86,Dept.Mech.Eng.,Uni.of Qld Brisbane,Australia,Dec.(1986).
    [8]
    卞荫贵、钟家康,《高温边界层传热》,科学出版社(1986).
    [9]
    徐立功、王中东,激波管乎衡边界层的数值解,中国科学技术大学学报,18,3(1988),352-358.
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