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Experimental study of fillets to reduce corner effects in an oblique shock-wave/boundary layer interaction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hirt, Stefanie M. |
| Copyright Year | 2015 |
| Description | A test was conducted in the 15 cm x 15 cm supersonic wind tunnel at NASA Glenn Research Center that focused on corner effects of an oblique shock-wave/boundary-layer interaction. In an attempt to control the interaction in the corner region, eight corner fillet configurations were tested. Three parameters were considered for the fillet configurations: the radius, the fillet length, and the taper length from the square corner to the fillet radius. Fillets effectively reduced the boundary-layer thickness in the corner; however, there was an associated penalty in the form of increased boundary-layer thickness at the tunnel centerline. Larger fillet radii caused greater reductions in boundary-layer thickness along the corner bisector. To a lesser, but measureable, extent, shorter fillet lengths resulted in thinner corner boundary layers. Overall, of the configurations tested, the largest radius resulted in the best combination of control in the corner, evidenced by a reduction in boundary-layer thickness, coupled with minimal impacts at the tunnel centerline. |
| File Size | 2299432 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20150002101 |
| Archival Resource Key | ark:/13960/t40s4s55h |
| Language | English |
| Publisher Date | 2015-01-05 |
| Access Restriction | Open |
| Subject Keyword | Fillets Corners Oblique Shock Waves Static Pressure Error Analysis Radii Shock Wave Generators Supersonic Wind Tunnels Upstream Shock Wave Interaction Temperature Measurement Tapering Thickness Wind Tunnel Tests Boundary Layers Mach Number Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |