Skip to main content
Log in

Effects of combustion on the interaction of an underexpanded wall hydrogen jet with a supersonic flow in a planar channel

  • Published:
Combustion, Explosion and Shock Waves Aims and scope

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.

Literature Cited

  1. V. K. Baev, V. I. Golovichev, et al., Combustion in a Supersonic Flow [in Russian], Nauka, Novosibirsk (1984).

    Google Scholar 

  2. E. Spiegler, M. Wolfstein, and R. Manheimer-Timnat, “A model of unmixedness for turbulent reacting flows,” Acta Astronautica,3, Nos. 3–4 (1976).

  3. O. M. Kolesnikov, “Effects of concentration pulsations on the ignition of a wall hydrogen jet in a supersonic flow,” Fiz. Goreniya Vzryva,21, No. 1 (1985).

  4. Y. C. Vigneron, J. V. Rakich, and J. C. Tannehill, “Calculation of supersonic viscous flows over delta wings with sharp subsonic leading edges,” AIAA Paper, 78-1137.

  5. M. Barnett and G. D. Power, “An efficient algorithm for strong viscous/inviscid interaction in hypersonic flows,” AIAA Paper, 88-0712.

  6. O. M. Kolesnikov, “Effects of the combustion of hydrogen in a supersonic boundary layer on the coefficient of friction,” Uch. Zap. TsAGT,19, No. 3 (1988).

  7. O. M. Kolesnikov, “Effects of hydrogen injection on the interaction of a nonequilibrium boundary layer with an external hypersonic flow,” Uch. Zap. TsAGI,18, No. 8 (1987).

  8. O. M. Kolesnikov, “Effects of underexpansion on the ignition delay for a wall hydrogen jet in a supersonic flow,” Fiz. Goreniya Vzryva,26, No. 5 (1990).

Download references

Authors

Additional information

Zhukovskii. Translated from Fizika Goreniya i Vzryva, Vol. 28, No. 6, pp. 11–17, November–December, 1992.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Kolesnikov, O.M. Effects of combustion on the interaction of an underexpanded wall hydrogen jet with a supersonic flow in a planar channel. Combust Explos Shock Waves 28, 581–586 (1992). https://doi.org/10.1007/BF00754864

Download citation

  • Received:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF00754864

Keywords

Navigation