What is it about?
Experimental data of ethylene combustion in supersonic flows are required for comparison with future numerical simulations. This work provides pressure distributions in a combustor for Mach 7-8 flight conditions (i.e. 7-8 times the speed of sound) as well as visualising the exhaust flame.
Featured Image
Read the Original
This page is a summary of: Fundamental Scramjet Combustion Experiments Using Hydrocarbon Fuel, Journal of Propulsion and Power, September 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b37472.
You can read the full text:
Contributors
Be the first to contribute to this page
