25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS 2006-2.4.5

DUAL-CODE SOLUTION PROCEDURE FOR EQUILIBRIUM HYPERSONIC AXISYMMETRIC TRANSITIONAL/TURBULENT FLOWS

K. Hejranfar, V. Esfahanian*, R. K. Moghadam
Sharif Univ. of Technology, Iran; *Univ. of Tehran, Iran

Keywords: Hypersonic Equilibrium Flows, Blunt-Body, Transitional/Turbulent Flows

A TLNS-PNS solution procedure is used to accurately and efficiently compute equilibrium hypersonic transitional/turbulent flows over blunt bodies. Both two codes are solved by the Beam-Warming algorithm using a shock fitting technique. The results are compared with available data and the real gas effects on the flowfield are studied.

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