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The role of freestream turbulence scale in subsonic flow separation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Potter, J. L. Seebaugh, W. R. Barnett, R. J. Gokhale, R. B. |
| Copyright Year | 1984 |
| Description | The ojective of this work is the clarification of the role of freestream turbulence scale in determining the location of boundary layer separation. An airfoil in subsonic wind tunnel flow is the specific case studied. Hot-film and hot-wire anemometry, liquid-film visualization and pressure measurements are the principal diagnostic techniques in use. The Vanderbilt University subsonic wind tunnel is the flow facility being used. |
| File Size | 5468816 |
| Page Count | 38 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850004562 |
| Archival Resource Key | ark:/13960/t45q9rv3v |
| Language | English |
| Publisher Date | 1984-12-31 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Boundary Layer Separation Turbulence Flow Distribution Hot-wire Anemometers Wind Tunnel Tests Flow Visualization Airfoils Velocity Distribution Hot-film Anemometers Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |