Loading...
Please wait, while we are loading the content...
Similar Documents
Experimental investigation of the application of microramp flow control to an oblique shock interaction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Anderson, Bernhard H. Hirt, Stefanie M. |
| Copyright Year | 2009 |
| Description | The effectiveness of microramp flow control devices in controlling an oblique shock interaction was tested in the 15- by 15-Centimeter Supersonic Wind Tunnel at NASA Glenn Research Center. Fifteen microramp geometries were tested varying the height, chord length, and spacing between ramps. Measurements of the boundary layer properties downstream of the shock reflection were analyzed using design of experiments methods. Results from main effects, D-optimal, full factorial, and central composite designs were compared. The designs provided consistent results for a single variable optimization. |
| File Size | 5708534 |
| Page Count | 33 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20090042751 |
| Archival Resource Key | ark:/13960/t3xt0pr69 |
| Language | English |
| Publisher Date | 2009-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Oblique Shock Waves Supersonic Wind Tunnels Shock Wave Interaction Experiment Design Spacing Factorial Design Boundary Layers Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
