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A computational-experimental development of vortex generator use for a transitioning s-diffuser
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wendt, Bruce J. Dudek, Julianne C. |
| Copyright Year | 1996 |
| Description | The development of an effective design strategy for surface-mounted vortex generator arrays in a subsonic diffuser is described in this report. This strategy uses the strengths of both computational and experimental analyses to determine beneficial vortex generator locations and sizes. A parabolized Navier-Stokes solver, RNS3D, was used to establish proper placement of the vortex generators for reduction in circumferential total pressure distortion. Experimental measurements were used to determine proper vortex generator sizing to minimize total pressure recovery losses associated with vortex generator device drag. The best result achieved a 59% reduction in the distortion index DC60, with a 0.3% reduction in total pressure recovery. |
| File Size | 918189 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19970009827 |
| Archival Resource Key | ark:/13960/t76t5m27g |
| Language | English |
| Publisher Date | 1996-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Navier-stokes Equation Drag Pressure Recovery Vortex Generators Distortion Analysis Mathematics Diffusers Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |