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Stall alleviation using a deformable leading edge concept
M. Sahin
*
, L. N. Sankar
*
Corresponding author for this work
Georgia Institute of Technology
Research output
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Contribution to journal
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Conference article
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peer-review
1
Citation (Scopus)
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Keyphrases
Airfoil
100%
Stall
100%
Deformable
100%
Alleviation
100%
Turbulence
16%
Two-layer
16%
Flow Field
16%
Surface Pressure Distribution
16%
Shape Change
16%
Superior Performance
16%
Second-order Accurate
16%
Helicopter Blade
16%
Integral Form
16%
Drag Characteristics
16%
NACA0012 Airfoil
16%
Low Drag
16%
Body-fitted Grid
16%
Pitching Moment
16%
Stall Characteristics
16%
Eddy-viscosity Model
16%
Integrated Load
16%
Dynamic Stall
16%
Two-dimensional Navier-Stokes Equations
16%
Engineering
Airfoil
100%
Leading Edge
100%
Two Dimensional
14%
Surface Pressure Distribution
14%
Shape Change
14%
Helicopter Blade
14%
Integral Form
14%
Eddy-Viscosity Model
14%
Pitching Moment
14%
Navier-Stokes Equation
14%
Flow Distribution
14%