Dual-Mode Operation and Transition in Axisymmetric Scramjets
Author:
Affiliation:
1. University of Illinois at Urbana-Champaign, Urbana, Illinois 61801
Funder
Air Force Office of Scientific Research
Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058391
Reference36 articles.
1. HesierW. H.PrattD. T., Hypersonic Airbreathing Propulsion, AIAA Education Series, AIAA, Washington, D.C., 1994, pp. 38–39, 334, 347–350. doi:10.2514/4.470356
2. CurranE. T.MurthyS. N. B., Scramjet Propulsion, Progress in Astronautics and Aeronautics, Vol. 189, AIAA, Reston, VA, 2001, p. 391. doi:10.2514/4.866609
3. Supersonic Combustion Processes
4. Unstart phenomena induced by flow choking in scramjet inlet-isolators
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