Abstract
A third-order-accurate upwind scheme is presented for solution of the steady two-dimensional Navier-Stokes equations in stream-function/vorticity form. The scheme is found to be accurate and stable at high Reynolds numbers. A series of test computations is performed on flows with large recirculating regions. In particular, highly accurate solutions are obtained for flow in a driven square cavity up to Reynolds numbers of 10**4. These computations are used to critically evaluate the accuracy of other existing first- and second-order-accurate upwind schemes. In addition, computations are carried out for flow in a channel with symmetric sudden expansion, flow in a channel with a symmetrically placed blunt base, and the flowfield of an impinging jet.
Original language | English |
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Journal | AIAA Paper |
State | Published - 1981 |
Event | AIAA Pap AIAA Aerosp Sci Meet, 19th - St Louis, MO, USA Duration: Jan 12 1981 → Jan 15 1981 |