Adaptive 3D single-block grids for the computation of viscous flows around wings
Conference
·
OSTI ID:416527
- National Aerospace Lab., Amsterdam (Netherlands)
A robust algorithm for the adaption of a 3D single-block structured grid suitable for the computation of viscous flows around a wing is presented and demonstrated by application to the ONERA M6 wing. The effects of grid adaption on the flow solution and accuracy improvements is analyzed. Reynolds number variations are studied.
- OSTI ID:
- 416527
- Report Number(s):
- CONF-960489--; CNN: Contract AERO-CT-0031
- Country of Publication:
- United States
- Language:
- English
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