An efficient multiblock method for aerodynamic analysis and design on distributed memory systems

Keyphrases

• Block Method 100%
• Aerodynamic Design 100%
• Distributed Memory System 100%
• Aerodynamic Optimization 100%
• Aerodynamic Analysis 100%
• Reynolds-averaged Navier-Stokes 66%
• Leonhard Euler 33%
• Adjoint Method 33%
• Design Process 33%
• Flow Model 33%
• Parallel Computer 33%
• Business Jet 33%
• Complex Configuration 33%
• Viscous Drag 33%
• Parallelizing 33%
• Lift Coefficient 33%
• Sample Calculations 33%
• Pylon 33%
• Parallel Performance 33%
• Message Passing Interface 33%
• Network of Workstations 33%
• Mesh Size 33%
• Aircraft Configuration 33%
• Horizontal Tail 33%
• Drag Minimization 33%
• Vertical Tail 33%
• Fixed Coefficients 33%
• Interface Standards 33%
• Wing-body 33%
• Nacelle 33%
• Flowing Solution 33%
• Design Optimization Problem 33%

Engineering

• Aerodynamic Design 100%
• Aerodynamic Analysis 100%
• Reynolds-Averaged Navier-Stokes 66%
• Design Optimization 66%
• Navier-Stokes Equation 66%
• Flow Model 33%
• Optimisation Problem 33%
• Flow Solution 33%
• Design Process 33%
• Mesh Size 33%
• Complete Aircraft 33%
• Aerodynamics 33%
• Parallel Computer 33%
• Jet 33%

Physics

• Aerodynamics 100%
• Navier-Stokes Equation 50%
• Design Optimization 50%
• Viscous Drag 25%