Unified Flow Solver for Aerospace Applications

Author:

Kolobov Vladimir1,Arslanbekov Robert1,Aristov Vladimir2,Frolova Anna2,Zabelok Sergey2

Affiliation:

1. CFD Research Corporation

2. Russian Academy of Sciences

Publisher

American Institute of Aeronautics and Astronautics

Reference20 articles.

1. Construction of a Unified Continuum/Kinetic Solver for Aerodynamic Problems

2. V.V.Aristov, A.A.Frolova, and S.A.Zabelok V.I.Kolobov, S.A.Bayyuk, R.R.Arslanbekov, inRAREFIED GAS DYNAMICS: 24th International Symposium on Rarefied Gas Dynamics, AIP Conference Proceedings 762, Monopoli, Bari, Italy, 10-16July 2004, page96

3. Direct Methods for Solving the Boltzmann Equation and Study of Nonequilibrium Flows

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1. Shock Structure Solution by Hybrid Flowfield Methods;Journal of Spacecraft and Rockets;2012-11

2. Towards the development of a hybrid statistical method for modeling reentry flows about blunt bodies;42nd AIAA Thermophysics Conference;2011-06-14

3. Hypersonic Blunt Body Thermophysics Using a Unified Kinetic/Continuum Solver;41st AIAA Thermophysics Conference;2009-06-14

4. Using the Unified Flow Solver to Investigate the Normal Shock Wave Structure;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

5. Unified Flow Solver Combining Boltzmann and Continuum Models for Simulations of Gas Flows for the Entire Range of Knudsen Numbers;Computational Fluid Dynamics 2006;2009

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