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The decay of longitudinal vortices shed from airfoil vortex generators
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Reichert, Bruce A. Wendt, Bruce J. Foster, Jeffry D. |
| Copyright Year | 1995 |
| Description | An experimental study is conducted to examine the crossplane structure and streamwise decay of vortices shed from airfoil-type vortex generators. The vortex generators are set in a counter-rotating array spanning the full circumference of a straight pipe. The span of the vortex generators above the duct surface, h, is approximately equal to the local turbulent boundary layer thickness, delta. Measurement of three-component mean flow velocity in downstream crossplanes are used to characterize the structure of the shed vortices. Measurements in adjacent crossplanes (closely spaced along the streamwise coordinate) characterize the interaction and decay of the embedded vortices. A model constructed by the superposition of Oseen vortices is compared to the data for one test case. |
| File Size | 920715 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19950022981 |
| Archival Resource Key | ark:/13960/t6353kf5h |
| Language | English |
| Publisher Date | 1995-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Computational Fluid Dynamics Oseen Approximation Ducts Flow Measurement Turbulent Boundary Layer Embedding Airfoils Counter Rotation Thickness Three Dimensional Flow Vortices Turbulence Models Vortex Generators Longitudinal Waves Flow Velocity Velocity Measurement Cross Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
