NASA NTRS · 19970011300
Progress in the Large-Eddy Simulation of an Asymmetric Plane Diffuser
Abstract
The flow through a plane asymmetric diffuser is a good test case for assessing the capability of LES since it contains features such as large scale unsteady separation and strong intermittency which are difficult to capture using conventional modeling approaches. Previous attempts to simulate this flow (Kaltenbach, 1994) have significantly underpredicted the extent of separation. The objective of the present research is to understand why the previous simulations did not predict the flow separation correctly. This study focuses on mesh refinement and matching of the inlet velocity profile. In order to perform this study, the flow solver of Kaltenbach (1994) was modified to increase its accuracy and efficiency. The improved algorithm allows for better resolution at affordable CPU cost.
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Fatica, Massimiliano, Mittal, Rajat. 1996-12-01. Progress in the Large-Eddy Simulation of an Asymmetric Plane Diffuser. https://ntrs.nasa.gov/citations/19970011300
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