Numerical Study on Thermodynamic Efficiency and Stability of Oblique Detonation Waves
Author:
Affiliation:
1. National University of Defense Technology, 410073 Changsha, People’s Republic of China
Funder
National Natural 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.J056887
Reference45 articles.
1. Morphology of standing oblique detonation waves
2. Approximate solutions for oblique detonations in the hypersonic limit
3. Oblique detonation wave engine performance prediction
4. Review of Propulsion Applications of Detonation Waves
5. Detonative propulsion
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