most citedNear-wall model for compressible turbulent boundary layers based on an inverse velocity transformation

44 citations · 46 across the 8 of their papers we have counts for

collaborators

8 papers

physics.flu-dyn2024

Non-equilibrium wall model for large eddy simulations of complex flows exhibiting turbulent smooth body separation

Rahul Agrawal, Sanjeeb T. Bose, Parviz Moin

In this work, a non-equilibrium wall model is proposed for the prediction of turbulent flows experiencing adverse pressure gradients, including separated flow regimes. The mean-flo…

physics.flu-dyn2024

Studies of Transonic Aircraft Flows and Prediction of Initial Buffet Onset Using Large-Eddy Simulations

Konrad A. Goc, Rahul Agrawal, Sanjeeb T. Bose +1

This article utilizes the Large-Eddy Simulation (LES) paradigm with a physics-based turbulence modeling approach, including a dynamic subgrid-scale model and an equilibrium wall mo…

physics.flu-dyn2024

Are the dynamics of wall turbulence in minimal channels and larger domain channels equivalent? A graph-theoretic approach

Ahmed Elnahhas, Emma Lenz, Parviz Moin +2

This work proposes two algorithmic approaches to extract critical dynamical mechanisms in wall-bounded turbulence with minimum human bias. In both approaches, multiple types of coh…

physics.flu-dyn2023

Reynolds number dependence of length scales governing turbulent flow separation with application to wall-modeled large-eddy simulations

Rahul Agrawal, Sanjeeb Bose, Parviz Moin

This article proposes a Reynolds number scaling of the required grid points to perform wall-modeled LES of turbulent flows encountering separation off a solid surface. Based on com…

physics.flu-dyn2023

An extension of Thwaites method for turbulent boundary layers

Rahul Agrawal, Sanjeeb T. Bose, Kevin P. Griffin +1

Thwaites (1949) developed an approximate method for determining the evolution of laminar boundary layers. The approximation follows from an assumption that the growth of a laminar…

physics.flu-dyn20232 cited

Large-eddy simulations of the NACA23012 airfoil with laser-scanned ice shapes

Brett Bornhoft, Suhas S. Jain, Konrad Goc +2

In this study, five ice shapes generated at NASA Glenn's Icing Research Tunnel (IRT) are simulated at multiple angles of attack (Broeren et al., J. of Aircraft, 2018). These geomet…