Summary
The cooling of a hot fluid in laminar Newtonian flow through cooled elliptic tubes has been calculated theoretically. Numerical data have been computed for the two values 1.25 and 4 of the axial ratio of the elliptic cross-section ε. For ε=1.25 the influence of non-zero thermal resistance between outmost fluid layer and isothermal surroundings has also been investigated. Special attention has been given to the distribution of heat flux around the perimeter; when ε increases the flux varies more with the position at the circumference. This positional dependence becomes less pronounced, however, as the (position-independent) thermal resistance of the wall increases.
Flattening of the conduit, while maintaining its cross-sectional area constant, improves the cooling. Comparison with rectangular pipes shows that this improvement is not as marked with elliptic as with rectangular pipes.
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Abbreviations
- A k =A m, n :
-
coefficients of expansion (6)
- a, b :
-
half-axes of ellipse, b<a
- a p =a r, s :
-
coefficients of representation (V)
- D :
-
hydraulic diameter, = 4S/P; S = cross-sectional area, P = perimeter
- D e :
-
equivalent diameter, according to (13)
- n :
-
coordinate (outward) normal to the tube wall
- T :
-
temperature of fluid
- T i :
-
temperature of fluid at the inlet
- T s :
-
temperature of surroundings
- v 0 :
-
mean velocity of fluid
- v z :
-
longitudinal velocity of fluid
- x, y :
-
carthesian coordinates coinciding with axes of ellipse
- z :
-
coordinate in flow direction
- α, β :
-
dimensionless half-axes of ellipse, α=a/D and β=b/D
- α t :
-
heat transfer coefficient from fluid at bulk temperature to surroundings; equation (11)
- α w :
-
heat transfer coefficient at the wall; equation (3)
- ε :
-
axial ratio of ellipse, = a/b = α/β
- ξ, η, ζ, ν :
-
dimensionless coordinates; ξ=x/D, η=y/D, ζ=z/D, ν=n/D
- ϑ :
-
dimensionless temperature, = (T−T s)/(T i−T s)
- ϑ 0 :
-
cup-mixing mean value of ϑ; equation (10)
- λ :
-
thermal conductivity of fluid
- μ m,n =μ k :
-
eigenvalue
- ρc :
-
volumetric heat capacity of fluid
- φ m, n =φ k =θ k :
-
eigenfunction; equations (6) and (I)
- Nu :
-
total Nusselt number, = α t D/λ
- \(Nu_\infty \) :
-
Nusselt number at large distance from the inlet
- Nu w :
-
wall Nusselt number, = α w D/λ, based on α w
- Pé:
-
Péclet number, = ν 0 Dρc/λ
References
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Schenk, J., Han, B.S. Heat transfer from laminar flow in ducts with elliptic cross-section. Appl. sci. Res. 17, 96–114 (1967). https://doi.org/10.1007/BF00419779
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DOI: https://doi.org/10.1007/BF00419779