Method for Predicting the Stability Limit to Acoustic Oscillations in Liquid-Propellant Rocket Engine Combustion Chambers Based on Combustion Noise.
| Autor: | Biryukov, V. I.1 (AUTHOR) aviatex@mail.ru, Ivanov, V. N.2 (AUTHOR), Tsarapkin, R. A.1,2 (AUTHOR) |
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| Zdroj: | Combustion, Explosion, & Shock Waves. Jan2021, Vol. 57 Issue 1, p74-82. 9p. |
| Databáze: | Academic Search Ultimate |
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