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Multiblock Navier Stokes method to simulate turbulent transonic flow over a delta-wing

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Thirteenth International Conference on Numerical Methods in Fluid Dynamics

Part of the book series: Lecture Notes in Physics ((LNP,volume 414))

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References

  1. Hilgenstock, A.: Validation of Transonic Turbulent Flows Past Delta Wing Configurations, Aero J., Aug/Sept 1991, pp.219–230.

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  2. Rizzi, A., Murman, E.M., Eliasson, P., and Lee, M.K.: Calculation of Hypersonic Leeside Vortices Over Blunt Delta Wings, in Vortex Flow Aerodynamics, AGARD CP-494, Paris 1990.

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  3. Vos, J.B. and Bergman, C.M.: A MultiBlock Flow Solver For Inviscid Hypersonic Flows, in Aerothermodynamics for Space Vehicles, (ed) B. Battrick, ESA SP-318 Noordwijk, 1991.

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  4. MEM-COM An Integrated Memory and Data Management System, MEM-COM User Manual Ver 5.6, SMR TR-5056, SMR Corp., Box 41, CH-2500 Bienne, 1988.

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  5. Becker, T.M.: Hybrid 3D Euler/Navier Stokes Calculations of Transonic Vortex Flows over the NTF Delta Wing, Masters Thesis, CFDL-TR-89-7, MIT, Cambridge, 1989.

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M. Napolitano F. Sabetta

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© 1993 Springer-Verlag

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Eldern, C., Vos, J., Rizzi, A., Oppelstrup, J. (1993). Multiblock Navier Stokes method to simulate turbulent transonic flow over a delta-wing. In: Napolitano, M., Sabetta, F. (eds) Thirteenth International Conference on Numerical Methods in Fluid Dynamics. Lecture Notes in Physics, vol 414. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-56394-6_259

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  • DOI: https://doi.org/10.1007/3-540-56394-6_259

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-56394-5

  • Online ISBN: 978-3-540-47551-4

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