Flow Choking Induced by Combustion and Mass Injection in a Circular Model Scramjet at Mach 4.5
Author:
Affiliation:
1. University of Tennessee, Knoxville
2. University of Illinois, Urbana-Champaign
Publisher
American Institute of Aeronautics and Astronautics
Reference47 articles.
1. B. One-Dimensional Treatment of Steady Gas Dynamics
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1. Numerical Simulation of Thermal Choking of a Channel during Combustion of a Hydrogen–Air Mixture in a Supersonic Flow;Combustion, Explosion, and Shock Waves;2023-08
2. PIV Measurements and Total Temperature Thermometry of a Mach 4.5 Arc-heated Nozzle Flow;AIAA SCITECH 2022 Forum;2022-01-03
3. Isolator Shock Dynamics of Mass Injection-Induced Unstart in a Circular Model Scramjet;23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2020-03-10
4. Pseudoshock Dimensionality in Axisymmetric and Rectangular Scramjets;AIAA Scitech 2020 Forum;2020-01-05
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