Difference between revisions of "Flows Around Bodies"

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| [[Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x10<sup>6</sup>)]] || [[University of Surrey]]
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| [[Flow around airfoils (and blades) A-airfoil (Ma=0.15, Re/m=2x10^6)]] || [[University of Surrey]]
 
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Revision as of 07:58, 23 May 2008