Implicit Velocity Correction Schemes for Scale-Resolving Simulations of Incompressible Flow: Stability, Accuracy, and Performance
Henrik W\"ustenberg, Alexandra Liosi, Spencer J. Sherwin, Joaquim Peir\'o, David Moxey

TL;DR
This paper compares implicit velocity correction schemes for high Reynolds number flow simulations, demonstrating they significantly extend stability limits and reduce overall computation time with minimal accuracy loss.
Contribution
It introduces and evaluates two implicit velocity correction methods, showing their advantages over standard semi-implicit schemes in stability and efficiency for complex geometries.
Findings
Implicit schemes extend stability limits by up to two orders of magnitude.
Overall time-to-solution is reduced by up to a factor of eleven.
Large time steps have minor impact on flow statistics and transition resolution.
Abstract
Scale-resolving simulations of high Reynolds number incompressible flows are often limited by the Courant-Friedrichs-Lewy (CFL) stability restriction imposed by explicit time-stepping schemes, resulting in small time step sizes and long time-to-solution. In this work, we systematically compare two implicit formulations of the velocity correction scheme -- a linear-implicit approach and a sub-stepping (or semi-Lagrangian) method -- against a standard semi-implicit formulation within a high-order spectral/hp element framework. The schemes are assessed in terms of stability limits, temporal accuracy, and computational performance for implicit large-eddy simulation of the Imperial Front Wing benchmark, a complex high Reynolds number geometry with curved surfaces that imposes strict CFL constraints. Both implicit schemes extend the stability limit by up to two orders of magnitude in time…
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