left-click = rotate, middle-button/CTLR-left-click = pan, scroll/right-click/ALT-left-click = zoom
|Description||This is a model of a standard propeller/wing CFD test case published in AGARD 303; case E6, configuration 2. The airfoil uses the published data points. The nacelle was constructed using FitModel to match the published data points as closely as possible. The data points are included in the model.|
2 - The source material used to create this model was Essentially Exact. This means detailed dimensions and drawings were used to create the model.