A delta wing has an aspect ratio of 1. (i) Plot the coefficients (K_{p}) and (K_{v}) with

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A delta wing has an aspect ratio of 1. 

(i) Plot the coefficients \(K_{p}\) and \(K_{v}\) with respect to Mach number  

(ii) for \(M=2\), plot the lift coefficient wrt angle of attack. Comment on the limiting values involved in the graph.

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