Calculation of three-dimensional low Reynolds number flows

An interactive boundary-layer stability-transition approach is used to calculate the performance characteristics of an infinite swept wing at low Reynolds numbers for several angles of attack. The research is discussed.

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Bibliographische Detailangaben
Veröffentlicht in:	Journal of aircraft 1994-05, Vol.31 (3), p.564-571
Hauptverfasser:	Cebeci, Tuncer, Chen, Hsun H, Lee, Beng P
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Applied fluid mechanics Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Laminar flows Low-reynolds-number (creeping) flows Physics
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Beschreibung
Zusammenfassung:	An interactive boundary-layer stability-transition approach is used to calculate the performance characteristics of an infinite swept wing at low Reynolds numbers for several angles of attack. The research is discussed.
ISSN:	0021-8669 1533-3868
DOI:	10.2514/3.46531