TY - GEN
T1 - High-Fidelity Versatile Incompressible Flow Solver for Direct Numerical Simulations and Linear Stability Investigations
AU - Hosseinverdi, Shirzad
AU - Fasel, Hermann F.
N1 - Funding Information:
This work was supported by the Air Force Office of Scientific Research (AFOSR) under grant number FA9550-19-1-0174, with Dr. Gregg Abate serving as the program manager. Computer time for numerical simulations was provided by the University of Arizona High Performance Computing center.
Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc. All rights reserved.
PY - 2022
Y1 - 2022
N2 - A high-fidelity versatile incompressible Navier-Stokes code was developed that is applicable for both Direct Numerical Simulations (DNS) and linear global stability investigations. The solver is based on a vorticity-velocity formulation of the Navier-Stokes equations for curvilinear orthogonal grids. It is programmed in Fortran 90 and employs parallelization using a hybrid MPI-OpenMP. The code incorporates advanced numerical algorithms, specially designed for simulations of transitional and turbulent flows. The solver includes linear stability modules based on the linearized Navier-Stokes equations (LNSE) that are tailored for primary and secondary instability investigations. No further assumptions are necessary (other than small amplitudes) with respect to the baseflow, and the primary wave as are required for conventional Linear Stability Theory (LST) and/or for Parabolic Stability Equations (PSE) analyses. Furthermore, since here the linear stability analysis is based on an initial value problem for LNSE, it is applicable for both convective and absolute/global instability with respect to both primary and secondary instability. An additional major advantage of the developed versatile solver is that linear/non-linear effects can be consistently evaluated by turning off/on the nonlinear terms. The new solver was employed for DNS of the flow for a wing section at a chord Reynolds number of Re = 200k. The capability of the linear stability modules was demonstrated by investigating the primary and secondary (convective & absolute) instability mechanisms for boundary layers and the flow past a circular cylinder.
AB - A high-fidelity versatile incompressible Navier-Stokes code was developed that is applicable for both Direct Numerical Simulations (DNS) and linear global stability investigations. The solver is based on a vorticity-velocity formulation of the Navier-Stokes equations for curvilinear orthogonal grids. It is programmed in Fortran 90 and employs parallelization using a hybrid MPI-OpenMP. The code incorporates advanced numerical algorithms, specially designed for simulations of transitional and turbulent flows. The solver includes linear stability modules based on the linearized Navier-Stokes equations (LNSE) that are tailored for primary and secondary instability investigations. No further assumptions are necessary (other than small amplitudes) with respect to the baseflow, and the primary wave as are required for conventional Linear Stability Theory (LST) and/or for Parabolic Stability Equations (PSE) analyses. Furthermore, since here the linear stability analysis is based on an initial value problem for LNSE, it is applicable for both convective and absolute/global instability with respect to both primary and secondary instability. An additional major advantage of the developed versatile solver is that linear/non-linear effects can be consistently evaluated by turning off/on the nonlinear terms. The new solver was employed for DNS of the flow for a wing section at a chord Reynolds number of Re = 200k. The capability of the linear stability modules was demonstrated by investigating the primary and secondary (convective & absolute) instability mechanisms for boundary layers and the flow past a circular cylinder.
UR - http://www.scopus.com/inward/record.url?scp=85123640000&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85123640000&partnerID=8YFLogxK
U2 - 10.2514/6.2022-1199
DO - 10.2514/6.2022-1199
M3 - Conference contribution
AN - SCOPUS:85123640000
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -