The design, construction, and tests of a concept aeroelastic wind tunnel model of a high-lift variable camber continuous trailing edge flap (HL-VCCTEF) wing configuration

Keyphrases

• Wind Tunnel Model 100%
• Design Test 100%
• High-lift 100%
• Aeroelasticity 100%
• Trailing Edge Flap 100%
• Variable Camber 100%
• Wing Configurations 100%
• Boeing 66%
• Trailing Edge 66%
• Nastran 66%
• Wind Tunnel 33%
• Mathematical Modeling 33%
• Aeroelastic Model 33%
• Aerodynamics 33%
• Development Effort 33%
• Mathematical Design 33%
• Physical Design 33%
• Design Challenges 33%
• Simulation Evaluation 33%
• Seattle 33%
• University of Washington 33%
• Flight Condition 33%
• Deflection 33%
• Control Surface 33%
• Degree of Control 33%
• Low-speed Wind Tunnel 33%
• Mathematical Modeling Method 33%
• Linear Finite Element 33%
• Noise Characteristics 33%
• Correlation Study 33%
• Aerodynamic Nonlinearity 33%
• Test Simulation 33%
• Control Mode 33%
• Physical Behavior 33%
• Aeroelastic Test 33%
• Aircraft Noise 33%
• Aeroelastic Behavior 33%
• Behavior Challenges 33%
• Control Degrees of Freedom 33%
• Aeroelastic Simulation 33%
• Leading-edge Slat 33%
• Panel Code 33%
• Fowler Flap 33%
• Moment Features 33%
• Test-analysis Correlation 33%
• Testing Program 33%

Engineering

• Construction Design 100%
• Flaps 100%
• Trailing Edge 100%
• Wind Tunnels 100%
• NASA 66%
• Mathematical Modeling 66%
• Aerodynamics 66%
• Degree of Freedom 33%
• Mode Control 33%
• Linear Finite Element 33%
• Physical Behavior 33%
• Test Analysis 33%
• Panel Code 33%
• Aeroelastic Behavior 33%
• Moment Characteristic 33%
• Design Method 33%
• Flight Condition 33%
• Leading Edge 33%
• Control Surfaces 33%
• Airframe 33%