FIRST-ORDER AND HIGHER-ORDER EFFECTS OF CURVATURE AND TORSION ON THE FLOW IN A HELICAL RECTANGULAR DUCT

Authors
Citation
Cj. Bolinder, FIRST-ORDER AND HIGHER-ORDER EFFECTS OF CURVATURE AND TORSION ON THE FLOW IN A HELICAL RECTANGULAR DUCT, Journal of Fluid Mechanics, 314, 1996, pp. 113-138
Citations number
55
Categorie Soggetti
Mechanics,"Phsycs, Fluid & Plasmas
Journal title
ISSN journal
00221120
Volume
314
Year of publication
1996
Pages
113 - 138
Database
ISI
SICI code
0022-1120(1996)314:<113:FAHEOC>2.0.ZU;2-J
Abstract
A series expansion method is employed to determine the first-order ter ms in curvature epsilon and torsion eta of fully developed laminar flo w in helical square ducts and in helical rectangular ducts of aspect r atio two. The first-order solutions are compared to solutions of the f ull governing equations. For toroidal square ducts with zero pitch, th e first-order solution is fairly accurate for Dean numbers, De = Re ep silon(1/2), up to about 20, and for straight twisted square ducts the first-order solution is accurate for Germane numbers, Gn = eta Re, up to at least 50 where Re is the Reynolds number. Important conclusions are that the flow in a helical duct with a finite pitch or torsion to the first order (i.e. with higher-order terms in epsilon and eta negle cted) is obtained as a superposition of the flow in a toroidal duct wi th zero pitch and a straight twisted duct; that the secondary flow in helical non-circular ducts for sufficiently small Re is dominated by t orsion effects; and that for increasing Re, the secondary flow eventua lly is dominated by effects due to curvature. Torsion has a stronger i mpact on the flow for aspect ratios greater than one. A characteristic combined higher-order effect of curvature and torsion is an enlargeme nt of the lower vortex of the secondary flow at the expense of the upp er vortex, and also a shift of the maximum axial flow towards the uppe r wall, For higher Reynolds numbers, bifurcation phenomena appear. The extent of a few solution branches for helical ducts with finite pitch or torsion is determined. For ducts with small torsion it is found th at the extent of the stable solution branches is affected little by to rsion. Physical velocity components are employed to describe the flow. The contravariant components are found useful when describing the con vective transport in the duct.