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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