TRANSITION PREDICTION FOR TRANSPORT AIRCRAFT CONFIGURATIONS BASED ON OVERSET GRID

Engineering

• Flight Condition 100%
• Transport Aircraft 100%
• Mach Number 50%
• Aerodynamic Design 50%
• High Reynolds Number 50%
• Good Agreement 50%
• Computational Fluid Dynamics 50%
• Laminar Flows 50%
• Leading Edge 50%
• Flow Simulation 50%
• Pressure Coefficient 50%
• Civil Aviation 50%
• Grid Generation 50%
• Great Importance 50%
• Civil Transport Aircraft 50%