Research and application of the continuous scan technique to the high angle of attack equipment in 8 m×6 m wind tunnel

Engineering

• Aircraft Model 50%
• Angle-of-Attack 100%
• Control System 50%
• Dynamic Pressure 50%
• Fighter Aircraft 50%
• Real-Time Control System 50%
• Test Data 50%
• Test Technique 50%
• Transport Aircraft 50%
• Tunnel 100%