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Unsteadiness in a ramjet model

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Combustion, Explosion, and Shock Waves Aims and scope

Abstract

The process of combustion of a hydrocarbon fuel in a pulsed mode is discussed on the basis of results of ramjet testing in an external flow modeling a Mach 5 flight.

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References

  1. S. Das and J. K. Prasad, “Behaviour of Flow Unsteadiness in a Supersonic Air-Intake with Throttles,” in Proc. 37th Int. and 4th National Conf. on Fluid Mechanics and Fluid Power, December 16–18, 2010, Madras, India.

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Authors and Affiliations

  1. Moscow Aviation Institute (National Research University), Moscow, 125993, Russia

    V. M. Levin, V. N. Karasev & L. L. Kartovitskii

  2. Bardin Central Research Institute of Ferrous Metallurgy, Moscow, 105005, Russia

    E. A. Krymov & O. A. Skachkov

Authors
  1. V. M. Levin
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  2. V. N. Karasev
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  3. L. L. Kartovitskii
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  4. E. A. Krymov
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  5. O. A. Skachkov
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Corresponding author

Correspondence to V. M. Levin.

Additional information

Original Russian Text © V.M. Levin, V.N. Karasev, L.L. Kartovitskii, E.A. Krymov, O.A. Skachkov.

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Translated from Fizika Goreniya i Vzryva, Vol. 49, No. 6, pp. 68–75, November–December, 2013.

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Levin, V.M., Karasev, V.N., Kartovitskii, L.L. et al. Unsteadiness in a ramjet model. Combust Explos Shock Waves 49, 682–689 (2013). https://doi.org/10.1134/S0010508213060075

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  • DOI: https://doi.org/10.1134/S0010508213060075

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