3. Linearised perturbation velocity potential equation for a 2-D wing in subsonic region, is: 0² 0² 02 + dy² (1-M²) Define limitations of the above equation. Can the equation be used for a wing, which flies at Moo> 1. Explain. = 0.
3. Linearised perturbation velocity potential equation for a 2-D wing in subsonic region, is: 0² 0² 02 + dy² (1-M²) Define limitations of the above equation. Can the equation be used for a wing, which flies at Moo> 1. Explain. = 0.
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