NUMERICAL COMPUTATION OF NONSTATIONARY AERODYNAMICS OF FLAT PLATE CASCADES IN COMPRESSIBLE FLOW.

Engineering

• Two Dimensional 100%
• Aerodynamics 100%
• Flat Plate 100%
• Numerical Computation 100%
• Compressible Flow 100%
• Amplitudes 50%
• Boundary Condition 50%
• Good Agreement 50%
• Accuracy 50%
• Phase Shift 50%
• Computational Domain 50%
• Slip Plane 50%
• Boundary Point 50%
• Dependent Variable 50%
• Fluid Property 50%
• Trailing Edge 50%
• Interior Point 50%
• Supersonic Flow 50%

Physics

• Calculation 100%
• Aerodynamics 100%
• Flat Plates 100%
• Plane 50%
• Boundaries 50%
• Steady State 50%
• Amplitudes 50%
• Domains 50%
• Boundary Condition 50%
• Region 50%
• Phase Angle 50%
• Wakes 50%
• Supersonics 50%