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A vortex entrainment model applied to slender delta wings (1974)

Coe, P. L., Jr.

In: Other Sources

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Publikationsdatum: 2011-08-16

Beschreibung: A mathematical model of the vortex flow over a slender sharp-edged delta wing is proposed, and is shown to provide good agreement with the experiment. Although the technique requires experimental data in the form of the vortex core locations, it does account for the previously ignored mass entrainment of the vortex core.

Schlagwort(e): AERODYNAMICS

Materialart: AIAA Journal; 12; Jan. 197

Format: text

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