Inclusion of Nonlinear Aerodynamics in the FLAP Code

Engineering

• Angle-of-Attack 100%
• Induced Velocity 100%
• Aerodynamics 100%
• Lift Coefficient 66%
• Tower 66%
• Solar Energy 33%
• Test Data 33%
• Aerodynamic Load 33%
• Horizontal Axis Wind Turbine 33%
• Compressed Air Motors 33%
• Iterative Procedure 33%
• Closed Form Solution 33%
• Field Test 33%
• Bending Moment 33%
• Drag Coefficient 33%
• Harmonics 33%