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Aircraft drag decomposition remains an important topic in aviation. This paper applies for the first time the concept of partial pressure fields (PPFs) to a transonic wing. It is shown that the recently developed theory on PPFs is an equivalent means of drag decomposition when compared to classical farfield methods.

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This page is a summary of: Drag Decomposition Using Partial-Pressure Fields: ONERA M6 Wing, AIAA Journal, December 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j061152.
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