Loading...
Please wait, while we are loading the content...
Similar Documents
An experimental documentation of trailing-edge flows at high reynolds number
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Seegmiller, H. L. Cleary, J. W. Viswanath, P. R. |
| Copyright Year | 1983 |
| Description | Experiments documenting attached trailing-edge and near-wake flows at high Reynolds numbers are described. A long, airfoil-like model was tested at subsonic and low transonic Mach numbers, and both symmetrical and asymmetrical flows with pressure gradients upstream of the trailing edge were investigated. Model surface pressures and detailed mean and turbulence flow qualities were measured in the vicinity of the trailing edge and in the near-wake. The data obtained are of sufficient quality and detail to be useful as test cases in assessing turbulence models and calculation methods. |
| File Size | 2291523 |
| Page Count | 48 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840002430 |
| Archival Resource Key | ark:/13960/t74v1fc46 |
| Language | English |
| Publisher Date | 1983-08-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Turbulent Flow Laser Doppler Velocimeters Subsonic Speed Reynolds Number Turbulent Boundary Layer Transonic Speed Airfoils Turbulence Models Flow Distribution Trailing Edges Wind Tunnel Tests Shear Stress Flow Visualization Near Wakes Symmetry Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
