Passive Flow Control on Civil Aircraft Flaps Using Sub-Boundary Layer Vortex Generators in the AWIATOR Programme
Author:
Affiliation:
1. Flight Physics, Airbus UK, Filton
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2858
Reference6 articles.
1. Investigation into Scale Effects on the Performance of Sub Boundary-Layer Vortex Generators on Civil Aircraft High-Lift Devices
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