Question
. An aircraft wing may be represented by a single horseshoe vortex of span 20 and circulation strength 25ms1. Calculate the downwash angle of
. An aircraft wing may be represented by a single horseshoe vortex of span 20 and circulation strength 25ms1. Calculate the downwash angle of a point 15 downstream of the bound vortex, in the plane of the vortex system on its centrelin The flight speed is 104 ms . (Answer: 0.4830).
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Applied Regression Analysis And Other Multivariable Methods
Authors: David G. Kleinbaum, Lawrence L. Kupper, Azhar Nizam, Eli S. Rosenberg
5th Edition
1285051084, 978-1285963754, 128596375X, 978-1285051086
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