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Chemically nonequilibrium laminar boundary layer in dissociated air

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Abstract

A difference scheme which permits computation without change in grid parameters over the entire range from equilibrium to frozen flow regimes is used to solve the equations of the chemically non-equilibrium boundary layer. Results are presented for the boundary layer in a mixture of N, O, NO, O2, and N2 with account for six reactions in the gaseous phase.

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References

  1. V. G. Gromov, “Use of a three-layer difference scheme for solving boundary layer equations,” Izv. AN SSSR, OTN, Mekhanika i mashinostroenie, no. 5, 1963.

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  3. Yun and Mason, “Collision integrals for the transport properties of dissociating air at high temperatures,” Phys. Fluids, vol. 5, no. 4, 1962.

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  5. K. Wray, “Chemical kinetics of high-temperature air,” in: Hypersonic Flow Research [Russian translation], Izd-vo Mir, 1964.

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  7. S. M. Gilinskii, G. F. Telenin, and G. P. Tinyakov, “Method of calculating supersonic flow about blunt bodies with separated shock,” Izd. AN SSSR, OTN, Mekhanika i mashinostroenie, no. 4, 1964.

  8. Yu. N. D'yakonov and N. A. Zaitseva, “Supersonic flow of an ideal gas about a blunt body,” Izv. AN SSSR, OTN, Mekhanika i mashinostroenie, no. 1, 1963.

  9. N. H. Kemp, P. H. Rose, and R. V. Detra, “Laminar heat transfer of blunt bodies with flow of dissociated air,” collection: Gasdynamics and Heat Transfer with Chemical Reactions [Russian translation], Izd. inostr. lit., 1962.

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Authors and Affiliations

  1. Moscow

    V. G. Gromov

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  1. V. G. Gromov
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In conclusion, I wish to thank G. I. Petrov, under whose guidance this study was carried out.

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Gromov, V.G. Chemically nonequilibrium laminar boundary layer in dissociated air. Fluid Dyn 1, 1–4 (1966). https://doi.org/10.1007/BF01013804

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  • DOI: https://doi.org/10.1007/BF01013804

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