Predictions of flow distortions inside a serpentine diffuser from large-eddy simulations
Rahul Agrawal, Chad Winkler, Sanjeeb Bose, Parviz Moin

TL;DR
This study uses large-eddy simulations to analyze flow separation and pressure distortions in a serpentine diffuser at various Mach numbers, achieving high accuracy in pressure recovery predictions and revealing non-local effects on flow separation.
Contribution
It demonstrates the effectiveness of advanced wall-modeled LES with dynamic tensor-coefficient Smagorinsky models in predicting flow distortions in complex diffuser geometries at different Mach regimes.
Findings
LES accurately predicts pressure recovery within 0.3%
LES captures azimuthal flow distortion within 7%
Simulations underestimate maximum azimuthal distortion and extreme events
Abstract
This work examines the flow separation and the resulting pressure distortions at the exit plane of a serpentine diffuser operating at both subsonic and transonic conditions. Wallmodeled large-eddy simulations (WMLES) using the charLES flow solver are performed at three exit-plane Mach numbers, Ma_AIP ~ {0.36, 0.46, 0.54}. First, it is shown that the onset of flow separation inside a serpentine diffuser may likely experience strong, non-local history effects. A grid refinement study consisting of five grids (from 30 million to 3 billion cells) is conducted for all Mach numbers. The recently proposed dynamic tensor-coefficient Smagorinsky subgrid-scale and sensor-aided non-equilibrium wall models compare favorably with experimental measurements for the pressure recovery and azimuthal flow distortion at all Mach numbers. The pressure recovery and azimuthal flow distortion are predicted to…
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Taxonomy
TopicsFluid Dynamics and Turbulent Flows · Heat Transfer Mechanisms · Aerodynamics and Acoustics in Jet Flows
