Influence of effective chemical reaction rate constants on the process of supersonic flow deceleration in a channel

Author:

Zamuraev V. P.,Kalinina A. P.

Publisher

AIP Publishing

Reference17 articles.

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3. Firsov A., V.I. Savelkin K. V. and et al., Philosophical Transactions: Mathematical, Physical and Engineering Sciences (Series A) 373, 20140337 (2015).

4. Three-dimensional modeling of rotating detonation in a ramjet engine

5. Numerical simulation of ethylene combustion in supersonic air flow

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Combustion initiation in a supersonic flow at various pressures, stagnation temperatures, and channel parameters;XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION;2023

2. Deceleration of a supersonic flow down to transonic speeds using gas-dynamic pulses during combustion of hydrocarbon fuels;AIP Conference Proceedings;2021

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