Large Eddy Breakup Devices as Low Reynolds Number Airfoils
- 1 October 1986
- proceedings article
- Published by SAE International
Abstract
No abstract availableThis publication has 25 references indexed in Scilit:
- The effects of drag reduction measures on boundary layer turbulence structure - Implications of an inviscid modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- The performance of smooth-wall drag reducing outer-layer devices in rough-wall boundary layersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Airfoil large-eddy breakup devices for turbulent drag reductionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Digital image filtering in visualized boundary layersAIAA Journal, 1984
- Body-turbulence interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Some experimental observations of the law of the wall behind large eddy breakup devices using servo-controlled skin friction balancesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Performance of large-eddy breakup devices at post-transitional Reynolds numbersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Turbulent drag reduction for external flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Alteration of outer flow structures for turbulent drag reductionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Drag reduction in turbulent boundary layers using ribbonsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982