Aeroelastic response of a panel under high speed turbulent boundary layers using direct numerical simulation

Keyphrases

• 3D Finite Element 33%
• Aeroelastic Response 100%
• Bending Wave 33%
• Boundary Layer 33%
• Compressible Navier-Stokes 33%
• Coupled Fluid-structure Interaction 33%
• Defection 33%
• Direct numerical Simulation 100%
• Finite Difference 33%
• Finite Element Solver 33%
• Fluid-structure Problem 33%
• Large Amplitude 33%
• Low Amplitude 33%
• Momentum Conservation 33%
• Momentum Equation 33%
• Navier-Stokes Solver 33%
• Panel Response 33%
• Solid Solution 33%
• Standing Wave 33%
• Thin Panel 33%
• Turbulence Statistics 33%
• Turbulent Boundary Layers 100%
• Wave Mode 33%
• Weak Shock 33%

Engineering

• Bending Wave 33%
• Boundary Layer 33%
• Compressible Navier 33%
• Direct Numerical Simulation 100%
• Finite Element Method 33%
• Momentum Equation 33%
• Panel Response 33%
• Solid Solution 33%
• Standing Wave 33%
• Turbulent Boundary Layer 100%
• Wall Unit 33%