Direct simulation Monte Carlo model of Low Reynolds number nozzle flows
- 1 July 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 10 (4) , 546-553
- https://doi.org/10.2514/3.23807
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Pressure measurements in a low-density nozzle plume for code verificationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- DSMC analysis of plume-freestream interactions and comparison of plume flowfield predictions with experimental measurementsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Time-derivative preconditioning for viscous flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Numerical and experimental investigations of rarefied nozzle and plume flows of nitrogenPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Analysis of large solid propellant rocket engine exhaust plumes using the direct simulation Monte Carlo methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Statistical collision model for Monte Carlo simulation of polyatomic gas mixtureJournal of Computational Physics, 1975
- Influence of Contraction Section Shape and Inlet Flow Direction on Supersonic Nozzle Flow and PerformanceJournal of Spacecraft and Rockets, 1972
- Supersonic nozzle discharge coefficients at low Reynolds numbersAIAA Journal, 1971
- Electron-beam studies of viscous flow in supersonic nozzlesAIAA Journal, 1971
- Comparison of measured and predicted flows through conical supersonic nozzles, with emphasis on the transonic regionAIAA Journal, 1965