Dynamic reattachment on a downward pitching finite wing

A finite wing was pitched downward at a constant rate from a fully stalled condition to zero angle of attack. Results from the test showed that dynamic reattachment initiation and progression velocity varied in response to alterations in nondimensional pitch rate and span location.

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Veröffentlicht in:Journal of aircraft 1996-03, Vol.33 (2), p.279-285
Hauptverfasser: Schreck, Scott J, Faller, William E, Luttges, Marvin W
Format: Artikel
Sprache:eng
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Zusammenfassung:A finite wing was pitched downward at a constant rate from a fully stalled condition to zero angle of attack. Results from the test showed that dynamic reattachment initiation and progression velocity varied in response to alterations in nondimensional pitch rate and span location.
ISSN:0021-8669
1533-3868
DOI:10.2514/3.46934