Dual-Mode Scramjet Control Using Optical Emission Sensors
Author:
Affiliation:
1. University of Virginia
2. Hampton University School of Science
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-0120
Reference29 articles.
1. A clean air continuous flow propulsion facility
2. Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder
3. Prediction of supersonic inlet unstart caused by freestream disturbances
4. Riley, L. P., Gaitonde, D. V., Hagenmaier, M. A., and Donbar, J. M. "Isolator dynamics during unstart of a dual-mode scramjet," American Institute of Aeronautics and Astronautics Inc. 2018, pp.1409-1427. https://doi.org/10.2514/1.B36888.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Dual-mode scramjet control using optical emission sensors;Applied Optics;2024-02-07
2. Potential for Closed-Loop Control of Dual-Mode Scramjets Using Optical Sensors;AIAA Journal;2023-11-29
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