Obtain the vortex lift line slope, given by Eq. 8.14, for a supersonic delta wing. Eq. 8.14
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Obtain the vortex lift line slope, given by Eq. 8.14, for a supersonic delta wing.
Eq. 8.14
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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