Airloads Correlation of the UH-60A Rotor inside the 40- by 80-Foot Wind Tunnel
Figure 12
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 speed sweep, Run 52 series. = 0.65 and /σ = 0.09.
