Development of a New CFD Multi-Coupling Tool Based on Immersed Boundary Method: toward SRM Analysis
The ongoing effort to develop an in-house
compressible solver with multi-disciplinary physics is presented in
this paper. Basic compressible solver combined with IBM technique
provides us an effective numerical tool able to tackle the physics
phenomena and especially physic phenomena involved in Solid
Rocket Motors (SRMs). Main principles are introduced step by step
describing its implementation. This paper sheds light on the whole
potentiality of our proposed numerical model and we strongly believe
a way to introduce multi-physics mechanisms strongly coupled is
opened to ablation in nozzle, fluid/structure interaction and burning
propellant surface with time.
[1] H. Bandringa, "Immersed boundary methods," Masterðôs thesis,
University of Groningen, vol. 9700, 2010.
[2] J. Yang and E. Balaras, "An embedded-boundary formulation for largeeddy
simulation of turbulent flows interacting with moving boundaries,"
Journal of Computational Physics, vol. 215, no. 1, pp. 12-40, 2006.
[3] C. P. T. Groth, D. L. De Zeeuw, K. G. Powell, T. I. Gombosi, and Q. F.
Stout, "A parallel solution-adaptive scheme for ideal
magnetohydrodynamics," 1999.
[4] D. E. Kooker and C. W. Nelson, "Numerical Solution of Three Solid
Propellant Combustion Models During a Gun Pressure Transient," Jan.
1977.
[5] I. Demirdžić, Ž. Lilek, and M. Perić, "A collocated finite volume
method for predicting flows at all speeds," International Journal for
Numerical Methods in Fluids, vol. 16, no. 12, pp. 1029-1050, 1993.
[6] M. Manna, A Three Dimensional High Resolution Upwind Finite
Volume Euler Solver. Von Karman Institute for Fluid Dynamics, 1992.
[1] H. Bandringa, "Immersed boundary methods," Masterðôs thesis,
University of Groningen, vol. 9700, 2010.
[2] J. Yang and E. Balaras, "An embedded-boundary formulation for largeeddy
simulation of turbulent flows interacting with moving boundaries,"
Journal of Computational Physics, vol. 215, no. 1, pp. 12-40, 2006.
[3] C. P. T. Groth, D. L. De Zeeuw, K. G. Powell, T. I. Gombosi, and Q. F.
Stout, "A parallel solution-adaptive scheme for ideal
magnetohydrodynamics," 1999.
[4] D. E. Kooker and C. W. Nelson, "Numerical Solution of Three Solid
Propellant Combustion Models During a Gun Pressure Transient," Jan.
1977.
[5] I. Demirdžić, Ž. Lilek, and M. Perić, "A collocated finite volume
method for predicting flows at all speeds," International Journal for
Numerical Methods in Fluids, vol. 16, no. 12, pp. 1029-1050, 1993.
[6] M. Manna, A Three Dimensional High Resolution Upwind Finite
Volume Euler Solver. Von Karman Institute for Fluid Dynamics, 1992.
@article{"International Journal of Engineering, Mathematical and Physical Sciences:64669", author = "Ho Phu TRAN and Frédéric PLOURDE", title = "Development of a New CFD Multi-Coupling Tool Based on Immersed Boundary Method: toward SRM Analysis", abstract = "The ongoing effort to develop an in-house
compressible solver with multi-disciplinary physics is presented in
this paper. Basic compressible solver combined with IBM technique
provides us an effective numerical tool able to tackle the physics
phenomena and especially physic phenomena involved in Solid
Rocket Motors (SRMs). Main principles are introduced step by step
describing its implementation. This paper sheds light on the whole
potentiality of our proposed numerical model and we strongly believe
a way to introduce multi-physics mechanisms strongly coupled is
opened to ablation in nozzle, fluid/structure interaction and burning
propellant surface with time.", keywords = "Compressible Flow, Immersed Boundary Method,
Multi-disciplinary physics, Solid Rocket Motors.", volume = "7", number = "4", pages = "660-5", }