Laminar, fully developed flow through single- and double-trapezoidal (or he
xagonal) ducts is modeled using a finite-difference method. A coordinate tr
ansformation is employed to map the irregular flow cross-section onto a rec
tangular computational domain. Both H1 and T thermal boundary conditions ar
e considered as they represent the fundamental limiting conditions in most
practical applications. Solutions for velocity and temperature variations a
re obtained for a wide range of duct aspect ratios and with four different
trapezoidal angles. The friction factor and Nusselt number results show a s
trong dependence on duct geometry (aspect ratio gamma and trapezoidal angle
theta). The variations off Re, Nu(H1), and Nu(T) With duct aspect ratio fo
r each theta-valued duct are presented in the form of polynomials in gamma.
These equations describe the computed numerical values within +/-2% for si
ngle-trapezoidal and within +/-1.5% for hexagonal ducts and are of much imp
ortance to the design of compact heat exchangers. (C) 1999 Elsevier Science
Ltd. All rights reserved.