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