- Category:
- Algorithm
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- File Size:
- 3kb
- Update:
- 2013-12-19
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- Uploaded by:
- 宋明健
Description: For the analysis of high Reynolds number flow around a cylinder naca0012 airfoils and basic available, but the numerical error, the error can be reduced by modifying certain parameters the
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naca0012-24-15.f90
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