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Nonequilibrium laminar boundary layer of dissociating air on axisymmetric bodies

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Abstract

Results are presented of numerical calculations of a nonequilibrium laminar boundary layer on axisymmetric bodies whose surface has arbitrary catalytic activity using a proposed technique. In the published studies devoted to the exact numerical methods for calculating the boundary layer with chemical reactions, it is assumed that the surface of the body is either noncatalytic or has infinite catalytic activity [1], that thermochemical equilibrium exists at the surface [2], or that the temperature and composition of the gas at the surface are given [3, 4]. This problem has been examined in the approximate formulation in several papers, specifically [5].

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References

  1. A. J. Pallone, J. A. Moore, and J. I. Erdos, “Nonequilibrium, nonsimilar solutions of the laminar boundary layer equations,” AIAA Journal, vol. 2, no. 10, 1964.

  2. V. G. Gromov, “Chemically nonequilibrium laminar boundary layer in dissociated air,” Izv. AN SSSR. MZhG [Fluid Dynamics], vol. 1, no. 2, 1966.

  3. F. G. Blottner, “Chemical nonequilibrium boundary layer,” AIAA Journal, vol. 2, no. 2, 1964.

  4. F. G. Blottner, “Nonequilibrium laminar boundary layer flow of ionized air,” AIAA Journal, vol. 2, no. 11, 1964.

  5. J. A. Fay and F. R. Riddell, “Theory of stagnation point heat transfer in dissociated air,” J. Aeronaut. Sci., vol. 25, no. 2, 1958.

  6. C. R. Wilke, “A viscosity equation of gas mixtures,” J. Chem. Phys., vol. 18, no. 4, 1950.

  7. K. S. Yan and E. A. Mason, “Collision integrals for the transport properties of dissociating air at high temperatures,” Phys. Fluids, vol. 5, no. 4, 1962.

  8. E. A. Mason and S. C. Saxena, “Approximate formula for the thermal conductivity of gas mixtures,” Phys. Fluids, vol. 1, no. 5, 1958.

  9. Sh.-Ch. Lin and J. D. Teare, “Rate of ionization behind shock waves in air, II; Theoretical interpretations,” Phys. Fluids, vol. 6, no. 3, 1963.

  10. Thermodynamic Properties of Individual Substances, Vol. 2 [in Russian], Izd-vo AN SSSR, Moscow, 1962.

  11. R. Goulard, “On catalytic recombination rates in hypersonic stagnation heat transfer,” Jet Propulsion, no. 11, 1958.

  12. I. N. Murzinov, “Laminar boundary layer on a sphere in hypersonic flow of equilibrium dissociating air,” Izv. AN SSSR. MZhG [Fluid Dynamics], vol. 1, no. 2, 1966.

  13. V. V. Lunev, V. G. Pavlov, and S. G. Sinchenko, “Hypersonic equilibrium dissociating air flow past a sphere,” Zh. vychisl. matem. i matem. fiz., vol. 6, no. 1, 1966.

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The authors wish to thank V. V. Lunev and I. N. Murzinov for their counsel and comments.

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Voronkin, V.G., Geraskina, L.K. Nonequilibrium laminar boundary layer of dissociating air on axisymmetric bodies. Fluid Dyn 4, 99–102 (1969). https://doi.org/10.1007/BF01025152

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  • DOI: https://doi.org/10.1007/BF01025152

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