Airloads Correlation of the UH-60A Rotor inside the 40- by 80-Foot Wind Tunnel
Figure 15
Comparison of predicted performance results (thrust, propulsive force, and power) of rotor/wind tunnel simulation (Prediction-WT) and NFAC test data (Test-NFAC) for the thrust sweep, Run 45 series. = 0.625 and μ = 0.3, = 0.0°.
