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Flat-plate transition
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ercegovic, B. A. |
| Copyright Year | 1985 |
| Description | A new research effort was undertaken to build a boundary-layer transition tunnel. This facility only recently became operational. The data obtained so far are merely qualitative. The main goal is to predict heat transfer given any combination of factors such as pressure gradient, turbulence level, Reynolds number, or intermittency factor. The boundary-layer transition tunnel is a closed-loop tunnel that controls the turbulence level, velocity and temperature of the air within it. Problems associated with the operation of this tunnel are examined. |
| File Size | 1332064 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850023125 |
| Archival Resource Key | ark:/13960/t8qc4wt9p |
| Language | English |
| Publisher Date | 1985-07-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Turbulence Reynolds Number Gas Turbine Engines Flow Distribution Wind Tunnel Tests Boundary Layer Transition Heat Transfer Pressure Gradients Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
