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AIAA Rotorcraft Hover Prediction Workshop (HPW)
AIAA Applied Aerodynamics Technical Committee
The S-76 Rotor Test Case
Calculations should be performed for a tip Mach number of 0.65 assuming standard day sea level conditions. To allow for direct comparison with other's results and to determine how well the investigator’s code captures the general trends it is recommended that the investigators cover the range of thrust conditions, nominally from CT/s = 0.02 to 0.10. Comparisons will also focus on the CT/s = 0.09 condition.
PLOT3D Surface Grids
Plot3D surface of the S-76 rotor blades are available on the FileShare page.
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