基于双e^N方法的短舱层流转捩影响因素

Engineering

• Mach Number 100%
• Reynolds' Number 100%
• Laminar Flows 100%
• Angle-of-Attack 100%
• Pressure Gradient 100%
• Influencing Factor 100%
• High Reynolds Number 50%
• Turbulence Intensity 50%
• Design Stage 50%
• Sideslip Angle 50%
• Attack Angle 50%
• Tollmien-Schlichting Wave 50%
• Linear Stability Analysis 50%
• Positive Pressure 50%
• Civil Transport Aircraft 50%