Numerical Simulation of High-Speed Non-equilibrium Flow with Applied Magnetic Field
https://doi.org/10.15514/ISPRAS-2017-29(6)-19
Abstract
The paper describes the development and testing processes of a modification of an existing solver for hypersonic reacting flow within the OpenFOAM numerical simulation framework. The modification is suited to simulate the interaction between the flow and the constant applied magnetic field. The purpose of the development is to create a simulation tool for the study of the concept of magnetohydrodynamical flow control and its possible technological applications. Resulting application utilizes Navier-Stokes-Fourier system of equations supplemented with appropriate auxiliary models for the accurate assessment of process-specific additional terms. Solver testing has been carried out using the cases that highlight solvers capabilities to model MHD high-speed flow in different regimes.
About the Authors
A. I. Ryakhovskiy
Ioffe Institute; Peter the Great St.Petersburg Polytechnic University
Russian Federation
Russian Federation
A. A. Schmidt
Ioffe Institute; Peter the Great St.Petersburg Polytechnic University
Russian Federation
Russian Federation
V. I. Antonov
Peter the Great St.Petersburg Polytechnic University
Russian Federation
Russian Federation
References
1. V. Bityurin, A. Bocharov, and J. Lineberry. MHD flow control in hypersonic flight. AIAA Paper, 3225, 2005.
2. T. Fujino, T. Yoshino, and M. Ishikawa. Numerical Analysis of Reentry Trajectory Coupled with Magnetohydrodynamics Flow Control. Journal of Spacecraft and Rockets, 45(5), 911, 2008.
3. N. Bisek, I. Boyd, and J. Poggie. Numerical study of plasma-assisted aerodynamic control for hypersonic vehicles. Journal of Spacecraft and Rockets, 46(3), 568, 2009.
4. E. Allen. The Case for Near Space. Aerospace America, February 2006,
5. A. Ryakhovskiy, and A. Schmidt. MHD supersonic flow control: OpenFOAM simulation. Trudy ISP RAN / Proc. ISP RAS, vol, 28, issue 1, 2016, pp. 197-206. DOI: 10.15514/ISPRAS-2016-28(1)-11
6. V. Casseau, R. Palharini, T. Scanlon, and R. Brown. A two-temperature open-source CFD model for hypersonic reacting flows, part one: zero-dimensional analysis. Aerospace, vol. 3(4), 2016.
7. I. Sarris, G. Zikos, A. Grecos, A. P., and N. Vlachos. On the limits of validity of the low magnetic Reynolds number approximation in MHD natural-convection heat transfer. Numerical Heat Transfer. Part B: Fundamentals, 50(2), pp. 157-180, 2006.
8. L. Spitzer and R. Härm. Transport phenomena in a completely ionized gas. Physical Review, 89(5), 977, 1953.
9. S. Chapman. and T. Cowling. The mathematical theory of non-uniform gases: an account of the kinetic theory of viscosity, thermal conduction and diffusion in gases. Cambridge university press, 1970.
10. Bush, W. B. Magnetohydrodynamic - Hypersonic Flow Past a Blunt Body. Journal of Aero/Space Sciences, Vol. 25, No. 11, November 1958, pp. 685-690.
11. Raizer, Y. P., Gas Discharge Physics, Springer-Verlag, 1991
12. S. Surzhikov. A computational study of aerothermodynamics of hypersonic flow around dull bodies using the example of analysis of experimental data. M.: IPMech, 2011, 74 p. (in Russian)
Review
For citations:
Ryakhovskiy A.I., Schmidt A.A., Antonov V.I. Numerical Simulation of High-Speed Non-equilibrium Flow with Applied Magnetic Field. Proceedings of the Institute for System Programming of the RAS (Proceedings of ISP RAS). 2017;29(6):299-310. https://doi.org/10.15514/ISPRAS-2017-29(6)-19
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