Deceleration of a supersonic flow down to transonic speeds using gas-dynamic pulses during combustion of hydrocarbon fuels
Author:
Publisher
AIP Publishing
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0052907
Reference9 articles.
1. Numerical studies and validation of combustor and annular isolator interactions of hydrocarbon based axisymmetric dual combustion ramjet
2. Two-stage fuel injection performance of RBCC under scramjet mode
3. Peculiarities of organization of effective hydrocarbon fuel combustion in supersonic flow
4. Organization of Effective Combustion of Kerosene in a Channel at High Flow Velocities
5. Initiation of Kerosene Combustion in a Supersonic Air Flow by a Bunch of Gas-Dynamic Pulses
Cited by 3 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 of Kerosene in a Supersonic Flow at Mach Number M = 1.7 Under the Action of Gas-Dynamical Pulses;Journal of Engineering Physics and Thermophysics;2023-07
2. Combustion of a hydrocarbon mixture in a supersonic flow at low Mach numbers;ACTUAL PROBLEMS OF CONTINUUM MECHANICS: EXPERIMENT, THEORY, AND APPLICATIONS;2023
3. Combustion of Ethylene and Kerosene in a Supersonic Flow at Low Mach Numbers;Combustion, Explosion, and Shock Waves;2022-08
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