Abstract
The heat transfer through an infinite flat plate is studied when the temperatures of the two free streams surrounding it are varying harmonically with time and out of phase, with a delay period τd. The configuration is a simplified model for the heat transfer through the separating wall in the isochoric counter-current heat exchanger. The results show that apart from the τd effect, the perturbation parameters depend mainly on the cavity passing frequency f. At the thick plate solution, the combined passing frequency–delay time influences are significant only when the dimensionless frequency is smaller than 10. Within this range τd affects seriously not only the temperature perturbation amplitudes (which determine the thermal stresses) but also the heat fluxes and the accumulated energy ones. When f ≥ 10, the plate behaves as two separate semi-infinite slabs. Heat penetration delays greater than one cavity passing period may be possible.
Similar content being viewed by others
Abbreviations
- A :
-
heat transfer surface
- a n , b n :
-
coefficients involved in the analytical solution
- B 1, B 2 :
-
Biot numbers
- B :
-
combined Biot number = B 1 + B 2
- B e :
-
effective Biot number (Eq. 14)
- c :
-
specific heat
- d :
-
penetration depth
- E :
-
accumulated energy
- f :
-
dimensionless frequency
- h :
-
heat transfer coefficient
- h tot :
-
overall heat transfer coefficient
- h p :
-
internal conductance of the plate per unit length
- k :
-
thermal conductivity
- L :
-
distance between the cavities
- P :
-
period
- p :
-
dimensionless period
- q :
-
heat flux
- T :
-
temperature
- T f1 :
-
temperature of fluid 1
- T f2 :
-
temperature of fluid 2
- t :
-
time
- t d :
-
delay period
- t k :
-
diffusion time
- u :
-
cavity velocity
- w :
-
plate thickness
- y :
-
transverse distance
- Y :
-
dimensionless y coordinate
- α:
-
thermal diffusivity
- β:
-
ratio of the overall heat transfer coefficient to the internal conductance per unit length of the plate = h tot/h p
- γ:
-
dimensionless amplitude of the temperature oscillation of the surrounding fluids
- δ:
-
dimensionless penetration depth
- ε :
-
dimensionless accumulated energy
- θ:
-
dimensionless temperature
- λ:
-
eigenvalues involved in the analytical solution
- ξ:
-
dimensionless time lag between the oscillation of the temperatures of the thick plate and the hot gas
- ρ:
-
mass density
- τ:
-
dimensionless time
- τd :
-
dimensionless delay period between the temperature oscillation of the surrounding fluids
- \({\tau_{0}^{*}, \tau_{\rm d}^{*}}\) :
-
dimensionless time lags between the oscillation of the temperatures of the thin plate and the hot gas
- φ:
-
dimensionless heat flux perturbation
- ψ:
-
phase difference between the oscillation of the temperatures of the thin plate and the hot gas
- Ω:
-
angular frequency
- ω:
-
dimensionless angular frequency
- 1:
-
side of the plate in contact with the fluid 1, at y = 0 (Y = 0)
- 2:
-
side of the plate in contact with the fluid 2, at y = w (Y = 1)
- 0:
-
initial
- amp:
-
amplitude
- mean:
-
mean value
- in:
-
entering the plate
- out:
-
exiting the plate
- qss:
-
quasi-steady (periodic) state
- step:
-
corresponding value when the free stream temperatures undergo step changes
- *:
-
thin plate
References
Carslaw HS, Jeager JC (1959) Conduction of heat in solids, 2nd edn. Oxford University Press, UK
Ehrhard P, Holle C, Karcher C (1993) Temperature and penetration depth prediction for a three-dimensional field below a moving heat source. Int J Heat Mass Transf 36:3997–4008
Georgiou DP (1996) The travelling cascade constant volume heat exchanger in a gas turbine lead combined cycle. ASME international gas turbine and aeroengine congress, Birmingham, UK, Paper 96-GT-536
Georgiou DP (2000) Useful work and the thermal efficiency in the ideal Lenoir cycle with regenerative preheating. J Appl Phys 88:5981–5986
Georgiou DP, Siakavellas N (2002) The 1-D heat transfer through a flat plate exposed to out of phase step changes in the free stream temperatures. Heat Mass Transf 38:657–663
Grabas B, Dard-Thuret J, Laurent M (1994) Observation with infrared thermography in laser welding. J Phys IV, Colloque C4, pp 139–142
Hou ZB, Komanduri R (2000) General solutions for stationary/moving plane heat source problems in manufacturing and tribology. Int J Heat Mass Transf 43:1679–1698
Ozisik MN (1989) Boundary value problems of heat conduction. Dover, USA
Ozisik MN (1993) Heat conduction. Wiley, New York, pp 204–206
Schneider PJ (1973) Conduction, section no 3. In: Rohsenow W, Hartnett JP (eds) Handbook of heat transfer. McGraw-Hill, USA
Siakavellas NJ, Georgiou DP (2005) 1D heat transfer through a flat plate submitted to step changes in heat transfer coefficient. Int J Therm Sci 44:452–464
Torii S, Yang W-J (2005) Heat transfer mechanisms in thin film with laser heat source. Int J Heat Mass Transf 48:537–544
Whitaker S (1983) Fundamental principles of heat transfer. Krieger, Florida, pp 157–159
Author information
Authors and Affiliations
Corresponding author
Appendices
Appendix A
The initial thin plate temperature, \({T^{*}(t = 0) \equiv T_{0}^{*}}\) is obtained from Eq. 23 if we take into consideration that, at t = 0, we have T f1(t) = T 1, T f2(t) = T 2 and \({dT_{0}^{*}/ dt = 0}\) . Then, Eq. 23 yields: \({h_{2} (T_{2} - T_{0}^{*}) - h_{1} (T_{0}^{*} - T_{1}) = 0}\) and \({T_{0}^{*}}\) is obtained as:
The non-dimensional thin plate temperature, \({\theta^{*}(\tau) = (T^{*}(t) - T_{0}^{*})/(T_{2} - T_{1})}\) , yields:
If we use now Eqs. (41)–(43), and take into consideration equations (1) and (12), we obtain the non-dimensional form of Eq. 23, i.e. Eq. 24.
For the thick plate case, Eq. 5 yields:
At t = 0 it is dT 0/dy = constant and from the boundary conditions (3a) and (3b) we obtain:
The solution of the system of Eq. (46) yields the initial temperature distribution:
The B 1, B 2, B e,β are given by equations (12) and (14), while \({T_{0}^{*}}\) is the initial temperature in the thin plate limit, given by Eq. 41. If we use now Eqs. 44–(47) and take into consideration Eqs. 6a, and 6b, we obtain from Eqs. 2, (3a), (3b) and (4), the non-dimensional form of the thick plate equations, i.e. Eqs. (7), (8a), (8b) and (11) respectively.
Appendix B
We have to solve Eq. 7 with boundary conditions given by equations (8a) and (8b). If the equation is solved in the time interval 0 ≤ τ ≤ τd, the initial condition is
while, if the equation is solved in the time interval τ > τd it is:
By separating the time and space variables, it is demonstrated easily that the complete solution of the temperature function θ(Y, τ) is given in the form
where c n are unknown coefficients to be determined, \({\bar{\theta }(\lambda _{n}, \tau )}\) is the integral transform of θ(Y,τ) with respect to the space variable Y in the range 0 ≤ Y ≤ 1, defined as:
while Ψ (λ n ,Y) has the form
In fact, Ψ (λ n ,Y) is the eigenfunction of the following auxiliary eigenvalue problem
The coefficients c n are determined by taking into consideration the orthogonality of the eigenfunctions Ψ (λ n ,Y) and are given as:
By applying now the transform (51) we take the integral transform of Eq. 7
The term in the first member in Eq. 56 is evaluated by making use of the Green’s theorem and taking into consideration the boundary conditions (8a), (8b) and the corresponding ones for the auxiliary eigenvalue problem, (54a), (54b):
By substituting Eq. 57 into Eq. 56, the latter it is finally written as:
where we have put for brevity
The application of the integral transform (51) to the initial condition (48) or (49) yields the corresponding initial condition for Eq. 58:
if the equation is solved in the time interval 0 ≤ τ ≤ τd, and
if the equation is solved in the time interval τ > τd.
The simplest case is when there is no phase difference between the temperature oscillations of the two fluids. Then τd = 0 in Eq. 59 and the solution of Eq. 58 subjected to the transformed initial condition (60) is:
If we introduce now Eqs. 55, (52) and (62) into the general form of the solution, i.e. Eq. 50 we obtain the following solution
where the eigenvalues λ n are the positive roots of the transcendental equation (33) while the coefficients a n , b n are given by Eq. 34.
In the general case, the solution depends on the time interval considered:
-
(a)
In the time interval [0 ≤ τ ≤ τd], the initial condition is given by Eq. 48; so, the solution is given again by Eq. 63 but, the coefficients a n are set zero, since γ1 is zero within this time interval.
-
(b)
In the time interval [τ > τd], the initial condition is given by Eq. 49, where F(Y) = θ(Y, τd) is obtained from Eq. 63 for τ = τd and a n = 0. Then, the solution of Eq. 58 subjected to the transformed initial condition (61) is:
$$ \begin{aligned} \bar {\theta}(\lambda _{n}, \tau ) =& \frac{B_{1} \gamma _{1}}{\lambda _{n}^{2}}{\left[ {1 - \frac{\omega ^{2} }{{\lambda _{n}^{4} + \omega ^{2}}}{\rm e}^{- \lambda ^{2}_{n} (\tau - \tau _{\rm d})} - \frac{\lambda _{n}^{2}}{{{\sqrt {\lambda _{n}^{4} + \omega ^{2}}}}}\cos {\left( {\omega {\kern 1pt} \tau - \omega {\kern 1pt} \tau _{\rm d} - \tan ^{- 1} \frac{\omega}{{\lambda _{n}^{2}}}} \right)}} \right]} \\ & + \frac{{B_{2} \gamma _{2} {\left( {\cos \lambda _{n} + \frac{B_{1}}{{\lambda _{n}}}\sin \lambda _{n}} \right)}}}{{\lambda _{n}^{2}}}{\left[ {1 - \frac{\omega ^{2}}{{\lambda _{n}^{4} + \omega ^{2}}}{\rm e}^{- \lambda _{n}^{2} \tau} - \frac{\lambda _{n}^{2}}{{{\sqrt {\lambda _{n}^{4} + \omega ^{2}}}}}\cos {\left( {\omega {\kern 1pt} \tau - \tan ^{{- 1}} \frac{\omega}{{\lambda _{n}^{2}}}} \right)}} \right]} \end{aligned} $$(64)
If we introduce now Eqs. 55, 52 and 64 into the general form of the solution, i.e., Eq. 50, we obtain Eq. 32.
Rights and permissions
About this article
Cite this article
Siakavellas, N.J., Georgiou, D.P. Heat transfer due to harmonic variation in the free stream temperatures in a flat plate exposed on both sides. Heat Mass Transfer 43, 1107–1119 (2007). https://doi.org/10.1007/s00231-006-0198-3
Received:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s00231-006-0198-3