AVT-183 diamond wing flow field characteristics Part 1: Varying leading-edge roughness and the effects on flow separation onset
Autor: | Christian Breitsamter, Andreas Hövelmann, Florian Knoth |
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Rok vydání: | 2016 |
Předmět: |
020301 aerospace & aeronautics
Engineering Leading edge Turbulence business.industry Aerospace Engineering Wing configuration 02 engineering and technology Mechanics 01 natural sciences 010305 fluids & plasmas Vortex Aerodynamic force Flow separation 0203 mechanical engineering 0103 physical sciences Surface roughness business Simulation Wind tunnel |
Zdroj: | Aerospace Science and Technology. 57:18-30 |
ISSN: | 1270-9638 |
DOI: | 10.1016/j.ast.2016.01.002 |
Popis: | Experimental investigations on a 53° leading-edge sweep diamond wing configuration with rounded leading-edge contour are presented. The analyses pertain to recent work that was conducted within the NATO Science and Technology Organization (STO) task group AVT-183 (Applied Vehicle Technology panel). The results were obtained in a low-speed wind tunnel facility and include aerodynamic forces and moments, and time-averaged surface pressures. Special emphasis is placed on the effects of different surface roughness, which was applied in the experimental analyses at the wing leading edge to fix turbulent boundary-layer characteristics. The results show that the flow separation onset and the emerging leading-edge vortex are very sensitive to the roughness height and any leading-edge contour modification. Compared to the free transition case, both reasonably-tripped and over-tripped cases are obtained, which is discussed in detail. Moreover, measurement repeatability issues are reviewed from a short-term and a long-term perspective. As an outcome, one specific leading-edge roughness is selected for the target flow conditions, which provided the baseline for subsequent flow field investigations and general CFD validation within the task group AVT-183. |
Databáze: | OpenAIRE |
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