Literature cited
H. K. Cheng, “Hypersonic shock-layer theory of the stagnation region at low Reynolds number,” Proc. Heat Transfer and Fluid Mech. Inst., Stanford (1961).
H. K. Cheng, “The blunt body problem in hypersonic flow at low Reynolds number,” J. Astronaut. Sci., No. 92 (1963).
L. I. Sedov, M. P. Mikhailova and G. G. Chernyi, “On the influence of viscosity and heat conductivity on gas flow behind a strongly curved shockwave,” Vestn. Mosk. Gos. Univ., Ser. Fiz.-Mat. Nauk, No. 3 (1953).
G. N. Zalogin and V. V. Lunev, “On the model of a viscous nonequilibrium shock layer with a thin shockwave,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 5 (1973).
A. S. Gorinov and K. M. Magomedov, “Method of splitting for the solution of relaxation equations in the presence of diffusion,” Zh. Vychisl. Mat. Mat. Fiz.,13, No. 5 (1973).
É. A. Gershbein, “Asymptotic investigation of the problem of spatial hypersonic viscous gas flow around blunt bodies with a permeable surface,” Hypersonic Spatial Flow in the Presence of Physicochemical Transformations [in Russian], Moscow (1981).
É. A. Gershbein, V. S. Shchelin, and S. A. Yunitskii, “Investigation of the spatial flow around bodies with a catalytic surface during their motion in earth's atmosphere,” Kosm. Issled., No. 3 (1985).
G. A. Tirskii, “On the theory of hypersonic flow around plane and axisymmetric blunt bodies by a viscous chemically reacting gas in the presence of blowing,” Tr. Inst. Mekh., Mosk. Cos. Univ. [in Russian], No. 39 (1975).
É. A. Gershbein and V. G. Shcherbak, “Investigation of hypersonic spatial flow around blunt bodies within the framework of parabolized Navier-Stokes equations,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4 (1987).
H. C. Kao, “Hypersonic viscous flow near the stagnation streamline of a blunt body,” AIAA J.,2, No. 11 (1964).
I. V. Petukhov, “Numerical analysis of two-dimensional flows in the boundary layer,” Numerical Methods of Solving Differential and Integral Equations and Quadrature Formulas [in Russian], Moscow (1964).
R. V. Masek, D. Hender, and J. A. Forney, “Evaluation of aerodynamic uncertainties for the space shuttle,” AIAA Paper No. 737, New York (1978).
C. D. Scott, “Catalytic recombination of nitrogen and oxygen on high-temperature reusable insulation,” AIAA Paper No. 1477, New York (1980).
Author information
Authors and Affiliations
Additional information
Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 1, pp. 49–56, January–February, 1989.
The author is grateful to G. A. Tirskii for constant attention to the research.
Rights and permissions
About this article
Cite this article
Shcherbak, V.G. Boundary conditions on a shock wave in a supersonic flow. J Appl Mech Tech Phys 30, 45–52 (1989). https://doi.org/10.1007/BF00860703
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF00860703