Wake integration for three-dimensional flowfield computations: Applications
A momentum balance approach is used to extract lift and drag from flowfield computations for wings and wing/bodies in subsonic/transonic flight. The drag is decomposed into vorticity, entropy, and enthalpy components that can be related to the established engineering concepts of induced drag, wave a...
| Main Authors: | , , |
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| Format: | Journal article |
| Language: | English |
| Published: |
1999
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