A two-dimensional boundary layer model for combustion chamber simulation
Author:
Funder
Conselho Nacional de Desenvolvimento Científico e Tecnológico
Coordenação de Aperfeiçoamento de Pessoal de Nível Superior
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s40430-024-04843-9.pdf
Reference19 articles.
1. Cheng GC, Farmer R (2006) Real fluid modeling of multiphase flows in liquid rocket engine combustors. J Propul Power 22(6):1373–1381
2. Chin JS, Lefebvre AH (1983) Steady-state evaporation characteristics of hydrocarbon fuel drops. AIAA J 21(10):1437–1443
3. Haidn OJ (2001) 2nd international workshop on rocket combustion modeling. DLR and European Office of Aerospace Research and Development, DLR, Langer Grund Lampoldshausen, Germany
4. Kalmykov GP, Larionov AA, Sidlerov DA, Yanchilin LA (2009) Numerical simulation of operation processes in the combustion chamber and gas generator of oxygen-methane liquid rocket engine. Prog Propul Phys 1:185–204
5. Kang YD, Sun B (2011) Numerical simulation of liquid rocket engine thrust chamber regenerative cooling. J Thermophys Heat Transf 25(1):155–164
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