Optimum aerodynamic design using the Navier-Stokes equations

Keyphrases

• Aerodynamic Design 100%
• Boundary Shape 100%
• Design Cycle 100%
• Transport Aircraft 50%
• Aerodynamic Shape Design 50%
• Viscous Compressible Flow 50%
• Long-range Transport 50%
• Wing-body Configuration 50%
• Inviscid Flow 50%
• Optimum Solution 50%

Engineering

• Design Cycle 100%
• Aerodynamic Design 100%
• Compressible Flow 50%
• Shape Design 50%
• Inviscid Flow 50%
• Flow Solution 50%
• Transport Aircraft 50%
• Optimum Solution 50%