For the attached flows over slender delta wings, show that at low angles of attack Eqs. 1.11
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For the attached flows over slender delta wings, show that at low angles of attack Eqs. 1.11 and 1.33 are identical.
Eq 1.11
Eq 1.13
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Related Book For 
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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