Retrospective on the Common Research Model for Computational Fluid Dynamics Validation Studies

The development of a wing–body–nacelle–pylon–horizontal-tail configuration for a common research model is presented, with the focus on the aerodynamic design of the wing. A contemporary transonic s...

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[22]  Christopher W. Lum,et al.  Generation of Fullspan Leading-Edge 3D Ice Shapes for Swept-Wing Aerodynamic Testing , 2016 .

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