Aerodynamic analysis of helicopter side intake variants by full scale wind tunnel measurements

Keyphrases

• Helicopter 100%
• Aerodynamics 100%
• Aerodynamic Analysis 100%
• Wind Tunnel Test 100%
• Air Intake 100%
• Local Surface 50%
• Fluid Mechanics 50%
• Flight Condition 50%
• Operation Conditions 50%
• Forward Flight 50%
• Mass Flow Rate 50%
• Wind Tunnel Model 50%
• Helicopter Fuselage 50%
• Aerodynamic Optimization 50%
• Helicopter Control 50%
• Surface Pressure Distribution 50%
• Hovering Flight 50%
• Pressure Probe 50%
• Significant Trend 50%
• Duct System 50%
• Fuselage Section 50%
• Total Pressure Drop 50%
• Full-scale Model 50%
• Radial Fan 50%
• Venturimeter 50%
• Interface Planes 50%

Engineering

• Full Scale 100%
• Aerodynamic Analysis 100%
• Aerodynamics 100%
• Wind Tunnels 100%
• Pressure Probe 33%
• Forward Flight 33%
• Mass Flowrate 33%
• Wind Tunnel Test 33%
• Fluid Mechanics 33%
• Duct System 33%
• Surface Pressure Distribution 33%
• Venturi Meter 33%
• Pressure Drop 33%
• Flight Condition 33%
• Pressure Sensor 33%
• Scale Model 33%