Development and Application of A High-Fidelity Numerical Tool for Dynamic Analysis of Bladed Disc Systems with Underplatform Dampers in Aircraft Engine Turbines

Keyphrases

• Numerical Tools 100%
• Bladed Disk System 100%
• Underplatform Damper 100%
• Dynamic Analysis 100%
• Aircraft Engine 100%
• ABAQUS 66%
• Behavior Analysis 33%
• Friction Coefficient 33%
• Dry-friction Contact 33%
• Time-marching Algorithm 33%
• Engine Design 33%
• Future Aircraft 33%
• Mechanical Engineering 33%
• Time-domain Simulation 33%
• System Dynamics 33%
• Aerospace Engineering 33%
• Tool Use 33%
• Contact Element 33%
• Dynamic Behavior 33%
• Steady State 33%
• Nonlinearity 33%
• Excitation Amplitude 33%
• Harmonic Excitation 33%
• Computation Time 33%
• Computational Modeling 33%
• Python 33%
• Mechanical Systems 33%
• Parameter Variation 33%
• Frequency Step 33%
• Vibration Behavior 33%
• Excitation Coefficient 33%

Engineering

• Aircraft Engine 100%
• Abaqus 66%
• Mechanical Engineering 33%
• Aerospace Engineering 33%
• Nonlinearity 33%
• Parametric Study 33%
• Computational Time 33%
• Mechanical Systems 33%
• Dry Friction 33%
• Harmonic Excitation 33%
• Dynamic Behavior 33%
• Illustrates 33%
• Time Domain 33%
• Engine Design 33%
• Friction Coefficient 33%
• Frequency Domain 33%
• Systems Dynamics 33%
• Contact Element 33%
• Coefficient of Friction 33%