Air-argon dual loop gas turbine engine with pulse detonation combustion and water injection
Author:
Publisher
Springer Science and Business Media LLC
Subject
Multidisciplinary
Link
https://link.springer.com/content/pdf/10.1007/s12046-022-01893-4.pdf
Reference15 articles.
1. Mitrofanov V V and Zhdan S A 2004 Thrust performance of an ideal pulse detonation engine. Combust. Explos. Shock waves 40(4): 38–385
2. Roy G D, Frolov S M, Borisov A A and Netzer D W 2004 Pulse detonation propulsion: challenges, current status, and future perspective. Prog. Energy Combust. Sci. 30(6): 545–672
3. Cleopatra F C, Tudor Cuciuc and Ionut Porumble 2016 Evaluation of the Cycle averaged performances of a pulsed detonation engine based on thermodynamic cycle computations. ASME Turbo Expo 2016 - Turbo machinery Technical Conference and Exposition: GT2016-57310
4. Wu Y, Ma F and Yang V 2003 System performance and thermodynamic cycle analysis of air-breathing pulse detonation engines. J. Propuls. Power 19(4): 556–567
5. Ma F, Choi J Y and Yang V 2006 Propulsive performance of air-breathing pulse detonation engines. J. Propuls. Power 22(6): 1188–1203
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