Wake integration for three-dimensional flowfield computations: Theoretical development
This paper examines the analytical, experimental, and computational aspects of the determination of the drag acting on an aircraft in flight, with or without powered engines, for subsonic/transonic flow. Using a momentum balance approach, the drag is represented by an integral over a crossflow plane...
Main Authors: | Giles, M, Cummings, R |
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Format: | Journal article |
Language: | English |
Published: |
1999
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