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Les of high-reynolds-number coanda flow separating from a rounded trailing edge of a circulation control airfoil
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Nichino, Takafumi Hahn, Seonghyeon Shariff, Karim |
| Copyright Year | 2010 |
| Description | This slide presentation reviews the Large Eddy Simulation of a high reynolds number Coanda flow that is separated from a round trailing edge of a ciruclation control airfoil. The objectives of the study are: (1) To investigate detailed physics (flow structures and statistics) of the fully turbulent Coanda jet applied to a CC airfoil, by using LES (2) To compare LES and RANS results to figure out how to improve the performance of existing RANS models for this type of flow. |
| File Size | 2296034 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20110008161 |
| Archival Resource Key | ark:/13960/t3mw7ds5h |
| Language | English |
| Publisher Date | 2010-06-09 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics High Reynolds Number Body-wing Configurations Computational Fluid Dynamics Circulation Control Airfoils Lift Augmentation Navier-stokes Equation Flow Equations Large Eddy Simulation Turbulence Models Trailing Edges Reynolds Averaging Coanda Effect Wing Profiles Turbulent Jets Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |
