Computational study of NOx formation in hydrogen-fuelled pulse detonation engines
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Publication:5900276
DOI10.1080/13647830600876629zbMath1141.80012OpenAlexW2035539434MaRDI QIDQ5900276
Sunhee Yoo, Bradley L. Wescott, D. Scott Stewart
Publication date: 3 September 2008
Published in: Combustion Theory and Modelling (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1080/13647830600876629
Multistep, Runge-Kutta and extrapolation methods for ordinary differential equations (65L06) Combustion (80A25) Chemically reacting flows (80A32)
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Cites Work
- Structure and stability of one-dimensional detonations in ethylene-air mixtures
- A fully implicit time accurate method for hypersonic combustion: Application to shock-induced combustion instability
- Detailed mechanism of the unsteady combustion around hypersonic projectiles
- Computational study of NOx formation in hydrogen-fuelled pulse detonation engines
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