A far-field drag prediction and decomposition method has been applied to the results of AIAA Drag Prediction Workshop 5 (DPW-5) held in Louisiana during the summer of 2012. The method has two principal advantages: it allows the removal of spurious drag inherent to CFD solutions, and it allows the decomposition of drag into viscous, wave, and induced physical drag components. This research shows that accurate drag coefficients can be predicted on coarse grids when the spurious drag is extracted with the far-field method, and that these results are closer to experimental values than drag coefficients computed on finer meshes when spurious drag is not extracted. The research also investigated the reasons behind the lift and drag losses found by some participants in the Workshop. It is shown that the lift loss is caused by the boundary layer separation at the wing root, inducing a reduction of 20% of the shock wave drag and a significant change in wing loading. The initiation of buffet is also analyzed. The study shows that mesh refinement is critical to capture the physical effects of the flow, such as its separation, and provides an explanation of the discrepancies in results observed at DPW-5.
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