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Maintenance of operational stability in liquid-propellant rocket engines by adjusting the acoustic properties of the combustion chambers

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Abstract

In liquid-propellant rocket engines, acoustic absorbers must be used to improve the stability of the combustion chambers with respect to some likely vibrational modes.

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References

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Authors and Affiliations

  1. Keldysh Scientific Center, Moscow, Russia

    S. V. Mosolov

  2. Moscow Aviation Institute, Moscow, Russia

    V. I. Biryukov

Authors
  1. S. V. Mosolov
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  2. V. I. Biryukov
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Corresponding author

Correspondence to S. V. Mosolov.

Additional information

Original Russian Text © S.V. Mosolov, V.I. Biryukov, 2013, published in Vestnik Mashinostroeniya, 2013, No. 3, pp. 3–8.

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Mosolov, S.V., Biryukov, V.I. Maintenance of operational stability in liquid-propellant rocket engines by adjusting the acoustic properties of the combustion chambers. Russ. Engin. Res. 33, 313–318 (2013). https://doi.org/10.3103/S1068798X13060130

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  • DOI: https://doi.org/10.3103/S1068798X13060130

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