Airloads Correlation of the UH-60A Rotor inside the 40- by 80-Foot Wind Tunnel
Figure 16
Comparison of predictions of free-air rotor only simulation (Prediction-Glauert), rotor/wind tunnel simulation (Prediction-WT), NFAC test data (Test-NFAC), and Airloads flight test (Test-Flight) for the matched flight test condition, Run 47 Point 21. = 0.637, μ = 0.3, = −4.8°, = −4.2°, and /σ = 0.087.
