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File:Vtc rae2822 cp.png

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Surface pressure coefficient for RAE2822 airfoil at Mach=0.729, AOA=2.31 deg and Re=6.5 million

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current09:17, 16 September 2005Thumbnail for version as of 09:17, 16 September 20051,200×900 (14 KB)Praveen (Talk | contribs) (Surface pressure coefficient for RAE2822 airfoil at Mach=0.729, AOA=2.31 deg and Re=6.5 million)

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