Stabilized detonation for hypersonic propulsion

Parent resource - Stabilization of Detonation Waves

DOI - 10.1073/pnas.2102244118
Journal Name - Proc. Natl. Acad. Sci. U.S.A.
Publisher Name - Proceedings of the National Academy of Sciences
Document Type - journal-article

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Paper Abstract- Significance There is now an intensifying international effort to develop robust propulsion systems for hypersonic and supersonic flight. Such a system would allow flight through our atmosphere at very high speeds and allow efficient entry and exit from planetary atmospheres. The possibility of basing such a system on detonations, the most powerful form of combustion, has the potential to provide higher thermodynamic efficiency, enhanced reliability, and reduced emissions. This work reports a significant step in attaining this goal: the discovery of an experimental configuration and flow conditions that generate a stabilized oblique detonation, a phenomenon that has the potential to revolutionize high-speed propulsion of the future.


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C Ramakrishnan  

Hypersonics Enthusiast with a Passion for Music and Photography....

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