Adjoint optimization of volumetric sources in steady, supersonic flow: Energy addition

Engineering

• Supersonic Flow 100%
• Drag Reduction 100%
• Boundary Layer 50%
• Euler Equation 50%
• Conservation of Energy 50%
• Adjoint Equation 50%
• Airfoil 50%
• Source Term 50%
• Optimization Method 50%
• Pitching Moment 50%
• Aircraft 50%

Keyphrases

• Adjoint Solution 50%