Modeling, analysis, and control of MFC sandwiched laminate panel flutter with general layups and arbitrary boundary conditions

Keyphrases

• Macro Fiber Composite 100%
• Panel Flutter 100%
• Arbitrary Boundary Conditions 100%
• Lagrange Equation 66%
• Elastic Edge Restraints 33%
• Piston Theory 33%
• Legendre Polynomials 33%
• Assumed Modes 33%
• Forcing Term 33%
• Aerodynamic Loads 33%
• Non-conservative Force 33%
• Smart Panel 33%
• Smart Plate 33%
• Displacement Potential 33%
• Proportional Feedback Control 33%
• Velocity Feedback Control 33%
• Flutter Boundary 33%
• Flutter Analysis 33%
• Supersonic Aerodynamics 33%
• Rectangular Composite Plate 33%
• Macro Fiber Composite Actuator 33%

Engineering

• Lagrange Equation 50%
• Aerodynamic Load 25%
• Conservative Force 25%
• Discretized Equation 25%
• Legendre Polynomial 25%
• Orthogonality 25%