Find the spanwise variation of lift for a delta wing with sweep angle (60^{circ}) at (mathrm{M}=1.5) and
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Find the spanwise variation of lift for a delta wing with sweep angle \(60^{\circ}\) at \(\mathrm{M}=1.5\) and \(\mathrm{k}=0.2\), at simple harmonic plunge. (Use 50 Max box for a half wing).
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Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
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