STAR-CCM+ Hands on Tutorial | External Compressible Transonic Flow Modelling | ONERA M6 Wing

This video is about Star-CCM+ hands on tutorial for external compressible transonic flow modelling over Onera M6 wing geometry. It will guide you how to model and import the geometry within Star-CCM+ and then follow on to do the polyhedral meshing with viscous prism layers. Afterwards, the solver setup and boundary conditions used for external transonic flows. Finally the pos-processing to visualize and examine the results.
#cfd #starccm #meshing
Further details of wing geometry and test case can be found on following references:
1. Schmitt, V. and F. Charpin, "Pressure Distributions on the ONERA-M6-Wing at Transonic Mach Numbers," Experimental Data Base for Computer Program Assessment. Report of the Fluid Dynamics Panel Working Group 04, AGARD AR 138, May 1979.
2. Further details of Onera M6 Wing can be found below: www.grc.nasa.gov/WWW/wind/valid/m6wing/m6wing.html turbmodels.larc.nasa.gov/onerawingnumerics_val.htm…
3. Mani, M., J.A. Ladd, A.B. Cain, and R.H. Bush, "An Assessment of One- and Two-Equation Turbulence Models for Internal and External Flows", AIAA 97-2010, June 1997.