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Optimization of the double-slot blown airfoil with jet at the leading and trailing edges of the flap

open access: yesAIP Advances
An active lift augmentation technique combining trailing edge blowing and blown flap is explored in this study. A double-slot blown flap airfoil is designed based on NACA23015.
Songlin Xiang   +3 more
doaj   +1 more source

Morphing Airfoil Design for Enhanced Aerodynamic Performance

open access: yes
This thesis investigates the design and evaluation of a morphing airfoil mechanism to improve aerodynamic performance over a wide range of flight regimes.
Chaafi, Melek
core  

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