Influence of differential spoiler settings on the wake vortex characterization and alleviation
Experimental investigations using particle image velocimetry technique have been carried out for the evaluation of the differential spoiler setting capabilities in modifying the spanwise wing load and further reduce the wake vortex hazard. The aircraft half model (at high lift configuration) was inv...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
American Institute of Aeronautical and Astronautic
2010
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/6010/ http://irep.iium.edu.my/6010/ http://irep.iium.edu.my/6010/ http://irep.iium.edu.my/6010/1/Infulence_of_differential__spoiler_settings_on_the_wake_vortex.pdf |