TURBULATOR GEOMETRY INFLUENCE ON TRIPPING EFFECTIVENESS BASED ON LOW-SPEED WIND-TUNNEL DATA
Keywords:
Aerodynamics, Structures, Materials, DesignAbstract
An experiment was conducted to determine the relative tripping effectiveness of different turbulator-tape geometries. Oil-flow photographic data were obtained in a low-speed wind tunnel for the upper surface of a Wortmann FX-63-1.37 airfoil two-dimensional wing section. Meaningful flow visualization data were obtained for several turbulator geometries that demonstrate different degrees of effectiveness for each turbulator configuration tested. A statistical compilation of the data quantitatively illustrate increased tripping effectiveness for a specific configuration tested, over the standard Z-patterned tape currently in use.Downloads
Issue
Section
Articles
License
CLEARANCE AND LICENSE TO PUBLISH:
This paper is UNCLASSIFIED (for public reasons) and has been cleared by the appropriate agencies, company and government. This paper represents original work by the author(s). No portion of the material is covered by a prior copyright; or for any portion copyrighted, the author has obtained permission for its use.
I hereby license OSTIV to publish this paper and to use it for all of OSTIV's current and future publications uses.