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Alula-inspired leading edge device for low Reynolds number flight
Boris A. Mandadzhiev
, Michael K. Lynch
,
Leonardo P. Chamorro
, Aimy A. Wissa
Mechanical Science and Engineering
Aerospace Engineering
Biomedical and Translational Sciences
Research output
:
Chapter in Book/Report/Conference proceeding
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Conference contribution
Overview
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Dive into the research topics of 'Alula-inspired leading edge device for low Reynolds number flight'. Together they form a unique fingerprint.
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Engineering
Leading Edge
100%
Angle-of-Attack
100%
Drag Coefficient
75%
Lift Coefficient
75%
Reynolds' Number
50%
Vortex
50%
Airfoil
50%
Relative Angle
50%
Tunnel
50%
Unmanned Aerial Vehicle
25%
Drag Force
25%
Adaptability
25%
Force Transducer
25%
Trailing Edge
25%
Flaps
25%
Flow Turbulence
25%
Aerodynamic Effect
25%
Fixed Wings
25%
Lift Force
25%
Aerodynamic Surface
25%
Aerodynamic Performance
25%
Mean Chord
25%
Envelope Design
25%
Aerodynamics
25%
Keyphrases
Low Reynolds number
100%
Edge Devices
100%
Alula
100%
Drag Coefficient
25%
Angle of Attack
25%
Lift Coefficient
25%
Reynolds number
16%
Aerodynamics
16%
Tip Vortex
16%
Relative Angle
16%
Drag Force
8%
Deflection
8%
Strong Correlation
8%
Low Angle
8%
Wind Tunnel
8%
Force Transducer
8%
Flap
8%
Wind Tunnel Experiment
8%
S1223
8%
Tip Deflection
8%
First Digit
8%
Six-axis
8%
Deployable
8%
UAV
8%
Aerodynamic Effect
8%
Lift Force
8%
Airfoil
8%
High Angle of Attack
8%
Deflection Ratio
8%
Mid-span
8%
Slat
8%
Wing Shape
8%
Aerodynamic Performance
8%
Vortex Strength
8%
Wing Surface
8%
Cambered Airfoil
8%
Wing Leading Edge
8%
Fixed-wing Aircraft
8%
Wing Performance
8%
Very Low Speed
8%
Normalized Lift
8%
Design Envelope
8%
Bird Wing
8%
Wing Trailing Edge
8%
Low-turbulence Flow
8%