Abstract
In this article, a comparison is made between the robustness and efficiency of the CLEAR algorithm and the SIMPLE algorithm on nonorthogonal curvilinear coordinates for compressible flows. Thirteen different high-order convection schemes are employed in the calculations. Subsonic flow, transsonic flow, and supersonic flow in a channel with a circular arc bump and compressible flow in a Laval nozzle are used as test cases. The CLEAR algorithm shows huge potential to compute the transsonic flow in the Laval nozzle and high-speed compressible flows. Results with the ADBQUICKEST scheme, the HLPA scheme, and the MUSCL scheme are stable for both the compressible SIMPLE and CLEAR algorithms for all the mentioned cases.
| Original language | English |
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| Pages (from-to) | 133-161 |
| Number of pages | 29 |
| Journal | Numerical Heat Transfer, Part B: Fundamentals |
| Volume | 66 |
| Issue number | 2 |
| DOIs | |
| State | Published - 1 Aug 2014 |