Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x10^6): Difference between revisions

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Revision as of 15:00, 6 April 2009 (view source) Daveg (talk \| contribs) (Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x10^6) moved to Abstr:Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x10^6))	Latest revision as of 11:14, 12 May 2009 (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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