UFR 2-05: Difference between revisions

Latest revision as of 10:36, 18 January 2010

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Revision as of 10:28, 18 January 2010 (view source) Daveg (talk \| contribs) No edit summary ← Older edit		Latest revision as of 10:36, 18 January 2010 (view source) Daveg (talk \| contribs) (Redirecting to Abstr:Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x10^6))
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