Skip to main content
Log in

Shock layer radiation in hypersonic airflow past blunt bodies

  • Published:
Fluid Dynamics Aims and scope Submit manuscript

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

References

  1. A. A. Kon'kov, V. Ya. Neiland, V. M. Nikolaev, and Yu. A. Plastinin, “Problems of radiative heat transfer in hypersonic aerodynamics”, Teplofizika vysokikh temperatur, vol. 7, no. 1, 1969.

  2. L. M. Biberman, V. S. Vorob'ev, A. N. Lagar'kov, V. P. Stulov, G. F. Telenin, E. G. Shapiro, and I. T. Yakubov, “Airflow behind strong shock wave front with account for nonequilibrium ionization and radiation”, Izv. AN SSSR, MZhG [Fluid Dynamics], vol. 2, no. 6, 1967.

  3. V. P. Stulov and E. G. Shapiro, “Effect of radiation on heat transfer at the stagnation point of a blunt body”, Izv. AN SSSR, MZhG [Fluid Dynamics], vol. 4, no. 2, 1969.

  4. V. V. Bogolepov, Yu. G. El'kin, and V. Ya. Neiland, “Inviscid radiating gas flow past a blunt body”, Izv. AN SSSR, MZhG [Fluid Dynamics], vol. 3, no. 4, 1968.

  5. O. M. Belotserkovskii and V. N. Fomin, “Radiating gas flow in a shock layer”, Zh. vychislit. matem. i matem. fiz., vol. 9, no. 2, 1969.

  6. N. A. Anfimov and V. P. Shari, “Solution of the equations of motion of a selectively radiating gas in a shock layer”, Izv. AN SSSR, MZhG [Fluid Dynamics], vol. 3, no. 3, 1968.

  7. H. Hoshizaki and K. H. Wilson, “Convective and radiative heat transfer during superorbital entry”, Raketnaya tekhnika i kosmonavtika, vol. 5, no. 1, 1967.

  8. H. Hoshizaki and L. E. Lasher, “Convective and radiative heat transfer to an ablating body”, Raketnaya tekhnika i kosmonavtika, vol. 6, no. 8, 1968.

  9. L. M. Biberman and S. Ya. Bronin, “On the theory of heating in hypersonic flow past bodies”, Dokl. AN SSSR, vol. 182, no. 3, 1968.

  10. V. S. Avduevskii and A. V. Ivanov, “Rarefied gas flow near the forward stagnation point of a blunt body at hypersonic speeds”, Izv. AN SSSR, MZhG [Fluid Dynamics], vol. 3, no. 3, 1968.

  11. A. P. Stulov and L. I. Turchak, “Supersonic airflow past a sphere with account for vibrational relaxation”, Izv. AN SSSR, MZhG [Fluid Dynamics], vol. 2, no. 5, 1966.

  12. V. P. Stulov and G. F. Telenin, “Nonequilibrium supersonic airflow past a sphere”, Izv. AN SSSR, MZhG [Fluid Dynamics], vol. 1, no. 1, 1965.

  13. A. N. Kraiko, “Analytic representation of the thermodynamic functions of air”, Inzh. zh., vol. 4, no. 3, 1964.

  14. 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.

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

About this article

Cite this article

Stulov, V.P., Shapiro, E.G. Shock layer radiation in hypersonic airflow past blunt bodies. Fluid Dyn 5, 140–146 (1970). https://doi.org/10.1007/BF01015012

Download citation

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF01015012

Keywords

Navigation