Effects of fuel injection angle on mixing performance of scramjet pylon-cavity flameholder
Author:
Affiliation:
1. Department of Aerospace Engineering, Indian Institute of Space Science and Technology, Thiruvananthapuram, 695547 Kerala, India
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0026125
Reference60 articles.
1. Mixing-Controlled Supersonic Combustion
2. Research on supersonic combustion
3. Hypersonic Airbreathing Propulsion
4. Fluid Phenomena in Scramjet Combustion Systems
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