Simulation of an electro-mechanical ice protection system for aircraft structure based on ultrasonic guided wave

Keyphrases

• Ice Protection System 100%
• Aircraft Structure 100%
• Open Rotor 100%
• Ultrasonic Guided Waves 100%
• Propeller 66%
• Ice Accretion 66%
• Shear Stress 66%
• Carbon Fiber Reinforced Polymer 66%
• Environmental Impact 33%
• Computational Model 33%
• Optimum Parameters 33%
• Low Emission 33%
• Safety Incidents 33%
• Fuel Saving 33%
• Power Efficient 33%
• Safety Procedures 33%
• Electromechanical Techniques 33%
• Piezoelectric Actuator 33%
• De-icing 33%
• Adhesive Bond Strength 33%
• Aisle 33%
• Wave Propagation 33%
• Debonding 33%
• Rotor Blade 33%
• De-icing System 33%
• Aerodynamic Performance 33%
• Aviation Safety 33%
• Blade Structure 33%
• Ice Mass 33%
• Actuator 33%
• Aerodynamic Control 33%
• Finite Element Analysis 33%
• Ice Conditions 33%
• Excitation Parameters 33%

Engineering

• Propeller 33%
• Shear Strength 33%
• Piezoelectric Actuator 33%