problem14_83

University Physics with Modern Physics with Mastering Physics (11th Edition)

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14.83: The pressure difference, neglecting the thickness of the wing, is ), ( ) 2 1 ( 2 bottom 2 top v v ρ p - = and solving for the speed on the top of the wing gives . s m 133 ) m kg 20 . 1 ( Pa) 2000 ( 2 s) m 120 ( 3
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Unformatted text preview: 2 top = + = v The pressure difference is comparable to that due to an altitude change of about m, 200 so ignoring the thickness of the wing is valid....
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This document was uploaded on 02/05/2008.

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