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Burnout of high-temperature products of incomplete combustion in a supersonic stream with secondary injection of oxidizer

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Abstract

Results are discussed of an experimental study concerning the burnout of products of incomplete combustion in a supersonic stream by means of secondary injection of oxidizers HNO3 or N2O4.

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Literature cited

  1. A. Ferry, P. A. Libby, and V. Zakay, High Temperatures in Aeronautics, Pergamon Press (1963), pp. 55–118.

  2. Z. G. Shaikhtudinov and A. M. Rusak, Inzh. Fiz. Zh.,21, No. 5 (1971).

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Authors
  1. Z. G. Shaikhutdinov
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  2. A. M. Rusak
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  3. V. M. Klevanskii
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  4. I. S. Saburov
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  5. L. F. Shaikhinurova
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Additional information

Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 25, No. 2, pp. 197–203, August, 1973.

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Shaikhutdinov, Z.G., Rusak, A.M., Klevanskii, V.M. et al. Burnout of high-temperature products of incomplete combustion in a supersonic stream with secondary injection of oxidizer. Journal of Engineering Physics 25, 943–947 (1973). https://doi.org/10.1007/BF00829840

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  • DOI: https://doi.org/10.1007/BF00829840

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