Search NASA⌕ Search

NASA NTRS · 20000034932

Implementation of Advanced Two Equation Turbulence Models in the USM3D Unstructured Flow Solver

Abstract

USM3D is a widely-used unstructured flow solver for simulating inviscid and viscous flows over complex geometries. The current version (version 5.0) of USM3D, however, does not have advanced turbulence models to accurately simulate complicated flow. We have implemented two modified versions of the original Jones and Launder k-epsilon "two-equation" turbulence model and the Girimaji algebraic Reynolds stress model in USM3D. Tests have been conducted for three flat plate boundary layer cases, a RAE2822 airfoil and an ONERA M6 wing. The results are compared with those from direct numerical simulation, empirical formulae, theoretical results, and the existing Spalart-Allmaras one-equation model.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Wang, Qun-Zhen, Massey, Steven J., Abdol-Hamid, Khaled S.. 2000-04-01. Implementation of Advanced Two Equation Turbulence Models in the USM3D Unstructured Flow Solver. https://ntrs.nasa.gov/citations/20000034932

Cite the original work for its findings. Save a collection to share your selection of sources.