Higher Order Theory Across a Three-Dimensional Axially-Symmetrical Curved Shock Near the Stagnation Point

Zhu Yue-rui; Yao Zhao-kang

Article Contents

Article Navigation > Applied Mathematics and Mechanics > 1985 > 6(12): 1087-1099

Zhu Yue-rui, Yao Zhao-kang. Higher Order Theory Across a Three-Dimensional Axially-Symmetrical Curved Shock Near the Stagnation Point[J]. Applied Mathematics and Mechanics, 1985, 6(12): 1087-1099.

Citation:

Zhu Yue-rui, Yao Zhao-kang. Higher Order Theory Across a Three-Dimensional Axially-Symmetrical Curved Shock Near the Stagnation Point[J]. Applied Mathematics and Mechanics, 1985, 6(12): 1087-1099.

Citation:

Zhu Yue-rui, Yao Zhao-kang. Higher Order Theory Across a Three-Dimensional Axially-Symmetrical Curved Shock Near the Stagnation Point[J]. Applied Mathematics and Mechanics, 1985, 6(12): 1087-1099.

PDF( 687 KB)

Higher Order Theory Across a Three-Dimensional Axially-Symmetrical Curved Shock Near the Stagnation Point

Department of Engineering Mechanics, Shanghai Jiaotong University, Shanghai

Received Date: 1984-05-03
Publish Date: 1985-12-15

Abstract

Abstract

The next order conditions across a three-dimensional curved shock near stagnation point have been established, including the effects of heat conduction, viscosity and the shock structure. These shock conditions involve the local shock curvature in addition to its local inclination. Explicit results have been obtained for the correctional formulations in the mass flux across the shock, the stagnation enthalpy, the tangential component of velocity and the normal component of momentum flux.

FullText(HTML)

References(5)

References

[1]	Chow,R.and Ting Lu(丁汝),Higher order theory of curved shock,Polytechnic Institute of Brooklyn,Aug.(1960).Aeronautical Research Laboratory Contract,No.AF33(616) -6118,Project No.7064,Task No.70169.
[2]	Tsien,H.S.,The equation of gas dynamics,H.W.Emmons(Editor),Fundamentals of Gas Dynamics,Princeton University Press,Princeton,N.J.(1958).
[3]	Richard,V.M.,Mathematics Theory of Compressible Fluid Flow,Academic Press,Inc.New York(1958).
[4]	Morduchow,M.and P.A.Libby,On a complete solution of the one-dimensional flow equations of viscous,heat-conducting compressible gas,Journal of the Aeronautical Sciences,16,11,Nov.(1949).
[5]	Liebber,P.,F.Romano and H.Lew,Approximate solutions of shock waves in a steady,one-dimensional viscous and compressible gas,Journal of the Aeronautical Sciences,18,1,Jan.(1951).