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Application of micro-ramp flow control devices to an oblique shock interaction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hirt, Stefanie Anderson, Bernhard |
| Copyright Year | 2007 |
| Description | Tests are planned in the 15cm x 15cm supersonic wind tunnel at NASA Glenn to demonstrate the applicability of micro-ramp flow control to the management of shock wave boundary layer interactions. These tests will be used as a database for computational fluid dynamics (CFD) validation and Design of Experiments (DoE) design information. Micro-ramps show potential for mechanically simple and fail-safe boundary layer control. |
| File Size | 1017513 |
| Page Count | 19 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080012598 |
| Archival Resource Key | ark:/13960/t1ng9mn3m |
| Language | English |
| Publisher Date | 2007-10-30 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics Computational Fluid Dynamics Oblique Shock Waves Supersonic Wind Tunnels Shock Wave Interaction Experiment Design Boundary Layer Control Fail-safe Systems Boundary Layers Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |