Neural network prediction of three-dimensional unsteady separated flowfields

Unsteady surface pressures were measured on a wing pitching beyond static stall. The surface pressure measurements confirmed that the pitching wing generated a rapidly evolving, 3D unsteady surface pressure field.

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Bibliographische Detailangaben
Veröffentlicht in:	Journal of aircraft 1995-01, Vol.32 (1), p.178-185
Hauptverfasser:	Schreck, Scott J, Faller, William E, Luttges, Marvin W
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Applied fluid mechanics Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Physics
Online-Zugang:	Volltext
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Beschreibung
Zusammenfassung:	Unsteady surface pressures were measured on a wing pitching beyond static stall. The surface pressure measurements confirmed that the pitching wing generated a rapidly evolving, 3D unsteady surface pressure field.
ISSN:	0021-8669 1533-3868
DOI:	10.2514/3.46698