For the two-dimensional transonic flow, in the range of small disturbance theory, the flow can be considered
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For the two-dimensional transonic flow, in the range of small disturbance theory, the flow can be considered as irrotational under the following conditions:
Try to prove that if the above differential equations are transformed by u and v as independent variables instead of x and y, that is
The nonlinear equations in xy plane can be changed into linear equations in velocity plane
where Ma∞ is the incoming Mach number and V is the incoming velocity.
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