Jet-Driven Unstart Process of a Hypersonic Inlet with Ramp Mass Injection
Author:
Affiliation:
1. Beijing Power Machinery Institute, 100074 Beijing, People’s Republic of China
Funder
National Nature Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061392
Reference11 articles.
1. CurranE. T.MurthyS. N. B. (eds.), Scramjet Propulsion, AIAA Education Series, AIAA, Reston, VA, 2000, pp. 447–511.
2. Unstart phenomena induced by flow choking in scramjet inlet-isolators
3. Hypervelocity Fuel/Air Mixing in Mixed-Compression Inlets of Shcramjets
4. GehreR.WheatleyV.BoyceR. “Combustion Regimes in Inlet-Fueled, Low Compression Scramjets,” AIAA Paper 2015-3507, 2013. 10.2514/6.2015-3507
5. Hypervelocity Fuel/Air Mixing in a Shcramjet Inlet
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