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Kutta-Joukowski theorem in compressible flow

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Murmur

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Jan 30, 2007, 9:06:06 PM1/30/07
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Is Kutta Joukowski theorem still applicable in compressible (subsonic) flow?

In other words, does the same circulation produces the same lift at 0.2 and
0.8 mach (V being the same, of course)?


Marco


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