Fig. 1. Test set-up.
Fig. 2. Grid for flow simulation.
Fig. 3. Grid around propeller.
Fig. 4. Nominal wake at propeller plane.
Fig. 5. Averaged Velocity on propeller plane.
Fig. 6. Spectrum of forces on control surface.
Fig. 7. Numerical prediction result at the observer point.
Fig. 8. Directivity pattern of numerical prediction.
Fig. 9. Numerical and Experimental noise spectrum results.
Fig. 10. Pressure time signal at an arbitrary point on the blade surface.
Table 1. Dimensions of DARPA Suboff and E1619.
Table 2. LCT model test conditions.
Table 3. Self-propulsion solution.
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