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Experimental investigation of Gurney flaps
Mark D. Maughmer
, Götz Bramesfeld
Aerospace Engineering
Research output
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Contribution to journal
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peer-review
101
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Engineering
Gurney Flap
100%
Experimental Investigation
100%
Airfoil
75%
Angle-of-Attack
37%
Leading Edge
25%
Flaps
25%
Pitching Moment
25%
Peak Pressure
12%
Reynolds' Number
12%
Turbulent Boundary Layer
12%
Reduced Pressure
12%
Laminar Flows
12%
Layer Flow
12%
Boundary Layer
12%
Separation Point
12%
Maximum Lift Coefficient
12%
Middle Part
12%
Pressure Recovery
12%
Linear Dependency
12%
Aerodynamics
12%
Surface Pressure Distribution
12%
Wind Tunnels
12%
Keyphrases
Gurney Flap
100%
Airfoil
75%
Angle of Attack
37%
Flap
25%
Surface Pressure
25%
Pitching Moment
25%
Lower Surface
25%
Boundary Layer
12%
Reynolds number
12%
Aerodynamics
12%
Reduced Pressure
12%
Laminar Flow
12%
Turbulent Boundary Layer Flow
12%
Low Angle
12%
Separation Point
12%
Momentum Deficit
12%
Wind Tunnel Experiment
12%
Linear Dependence
12%
Maximum Lift Coefficient
12%
Pressure Recovery
12%
Aft-loading
12%
Pressure Peak
12%
Residual Gradient
12%
Surface Pressure Distribution
12%
Lift Enhancement
12%
Negative Lift
12%
Simple Device
12%
Low Speed Wind Tunnel
12%