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...

Szczegółowa specyfikacja

Opis bibliograficzny
Główni autorzy: Hunt, D, Cummings, R, Giles, M
Format: Journal article
Język:English
Wydane: 1999

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