Flow Control and High-Lift Performance for Flying-Wing Unmanned Combat Air Vehicle Configurations by inserting slots
The objectives of the present study on Unmanned Combat Air Vehicles (UCAVs) are two-fold: first to control the flow by inserting leading-edge and cross-flow slots and analysing the viscous flow development over the outer panels of a flying-wing configuration to maximise the performance of the elevon...
Main Authors: | U Ali, E Chadwick |
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Format: | Article |
Language: | English |
Published: |
MULTIPHYSICS
2016-06-01
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Series: | International Journal of Multiphysics |
Online Access: | http://journal.multiphysics.org/index.php/IJM/article/view/114 |
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