Interaction of a Mach 2.25 turbulent boundary layer with a fluttering panel using direct numerical simulation

Keyphrases

• Direct numerical Simulation 100%
• Turbulent Boundary Layers 100%
• Flutter 100%
• Boundary Layer 66%
• Bending Wave 66%
• Solid Solution 33%
• Finite Element Solver 33%
• Eigenmodes 33%
• Finite Difference 33%
• Standing Wave 33%
• Finite Deformation 33%
• Turbulent State 33%
• Low Amplitude 33%
• Limit Cycle 33%
• Layer's System 33%
• Navier-Stokes Solver 33%
• Wave Pattern 33%
• Coupled Fluid-structure Interaction 33%
• Turbulence Statistics 33%
• Fully Turbulent 33%
• 3D Finite Element 33%
• Fluid-structure Problem 33%
• Compressible Navier-Stokes 33%
• Finite Strain 33%
• Boundary Layer Transition 33%
• Laminar Boundary Layer 33%
• Panel Thickness 33%
• Numerical Simulation Approach 33%
• Integral Length 33%
• Sonic Line 33%
• Panel Deflection 33%
• Deformation Equation 33%
• Boundary Layer Profile 33%

Engineering

• Boundary Layer 100%
• Direct Numerical Simulation 100%
• Turbulent Boundary Layer 100%
• Bending Wave 66%
• Finite Element Method 33%
• Finite Deformation 33%
• Solid Solution 33%
• Eigenmode 33%
• Limit Cycle 33%
• Compressible Navier 33%
• Standing Wave 33%
• Finite Strain 33%
• Wall Unit 33%
• Boundary Layer Transition 33%
• Laminar Boundary Layer 33%
• Sonic Line 33%
• Panel Thickness 33%