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Second-moment rans model verification and validation using the turbulence modeling resource website (invited)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Togiti, Vamshi Eisfeld, Bernhard Rumsey Sr., Chris |
| Copyright Year | 2015 |
| Description | The implementation of the SSG/LRR-omega differential Reynolds stress model into the NASA flow solvers CFL3D and FUN3D and the DLR flow solver TAU is verified by studying the grid convergence of the solution of three different test cases from the Turbulence Modeling Resource Website. The model's predictive capabilities are assessed based on four basic and four extended validation cases also provided on this website, involving attached and separated boundary layer flows, effects of streamline curvature and secondary flow. Simulation results are compared against experimental data and predictions by the eddy-viscosity models of Spalart-Allmaras (SA) and Menter's Shear Stress Transport (SST). |
| File Size | 8769821 |
| Page Count | 47 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20160006056 |
| Archival Resource Key | ark:/13960/t7bs3sr9m |
| Language | English |
| Publisher Date | 2015-06-22 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics Reynolds Stress Laminar Flow Simulation Turbulence Models Shear Stress Computational Grids Separated Flow Eddy Viscosity Convergence Boundary Layer Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |