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Eq. 11 12 represents a combination of continuity, momentum, energy equations. In principle, it can be solved to obtain for the flow field around any two-dimensional flow The infinite boundary condition is ao=vo ax 0p=0 The wall boundary condition is 0p=0 anEq. 11.12 represents a combination of continuity, momentum, energy equations. In principle, it can be solved to obtain for the flow field around any two-dimensional flow. The infinite boundary condition is =    = V x u  = 0   = y v  The wall boundary condition is = 0   n  
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