Abstract
This paper deals with the analytical investigation of the steady-state heat conduction within a semi-infinite medium embedding an insulating penny-shaped crack and subjected to a disk heat source of an arbitrary heat flux distribution. This axisymmetric heat conduction problem is formulated as a mixed boundary value problem, which is then converted to dual integral equations using the Hankel integral transform technique. A solution approach based on the Gegenbauer addition formula is employed to directly reduce the resulting integral equations into an infinite set of simultaneous equations. Closed-form expressions for temperature, heat flux, heat flux intensity factor near the crack tip, and constriction resistance are subsequently derived. Moreover, four practical configurations of heat flux conditions are further investigated and discussed. Sets of dimensionless plots are provided to show the effect of the size and depth of the crack on the thermal fields, heat flux intensity factor, and constriction resistance. Additionally, the validity of the obtained results is tested by comparison with numerical simulations and shows a good agreement.
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Abbreviations
- a :
-
Radius of the heat spot, m
- \(A, A_j, B_j\) :
-
Unknown functions
- \(A_{mn}^\circ \) :
-
Matrix elements of the algebraic system
- b :
-
Radius of the penny-shaped crack, m
- \(b_m^\circ \) :
-
Vector elements of the right-hand side of the algebraic system
- c :
-
Dimensionless radius of the penny-shaped crack
- d :
-
Dimensionless depth of the penny-shaped crack
- E :
-
Complete elliptic integral of the second kind
- F :
-
Gauss hypergeometric function
- h :
-
Depth of the penny-shaped crack, m
- H :
-
Heaviside step function
- \(H_\nu \) :
-
Struve function of order \(\nu \)
- \(J_\nu \) :
-
Bessel function of the first kind of order \(\nu \)
- k :
-
Thermal conductivity, W/(m\(\cdot \)K)
- K :
-
Complete elliptic integral of the first kind
- \(K_T\) :
-
Heat flux intensity factor, \({\mathrm{W/m}^{3/2}}\)
- q :
-
Heat flux loading, \({\mathrm{W/m}^2}\)
- \(q_0\) :
-
Constant heat flux, \({\mathrm{W/m}^2}\)
- \(q_\textrm{t}\) :
-
Total heat flux over the contact area, W
- \(q_z\) :
-
Heat flux in the z-direction, \({\mathrm{W/m}^2}\)
- \(q_\zeta \) :
-
Dimensionless Heat flux in the \(\zeta \)-direction
- r, z :
-
Radial and axial coordinates, m
- \(R_\textrm{c}\) :
-
Thermal constriction resistance, K/W
- si:
-
Sine integral function
- T :
-
Dimensionless temperature
- \(T_n\) :
-
Chebyshev’s polynomials of the first kind of degree n
- \(U_n\) :
-
Chebyshev’s polynomials of the second kind of degree n
- \(\alpha _n\) :
-
Series coefficients
- \(\Gamma \) :
-
gamma function
- \(\delta _{\ell m}\) :
-
Kronecker delta
- \(\zeta , \rho \) :
-
Dimensionless axial and radial coordinates
- \(\theta \) :
-
Temperature, K
- \(\theta _{\textrm{av}}\) :
-
Average temperature of the contact area, K
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Acknowledgements
The support from Directorate-General for Scientific Research and Technological Development (DG-RSDT) of Algerian government in the form of research grant is gratefully acknowledged. The Laboratory of Green and Mechanical Development (LGMD) of National Polytechnic School (ENP) is also gratefully acknowledged for the resources and support.
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Appendices
Derivation of the integral formula (41)
From [45, Eq. (6.522 11)], it is easy to find that
where \(T_n\) is Chebyshev’s polynomials of the first kind of degree n defined by [45, Eq. (8.940 1)] \(T_n(x)=\cos (n\,\arccos \,x)\). Taking the difference between the \((n+1)\textrm{th}\) and \(n\textrm{th}\) equations and using the following recursion formulas [45, Eqs. (8.941 1 and 4)]
yield
Asymptotic expansion formulas of \(\scriptstyle {N_n}\) and \(\scriptstyle {Y_m}\)
For large values of \(\xi \), the asymptotic expansion of the Bessel function \(J_{\nu }\) reads [45, Eq. (8.451 1), \(\nu =1\)]
As \(M_n(\xi )=J_{n+1/2}\left( \xi \,c/2\right) \,J_{-n-1/2}(\xi \,c/2)\) and \(X_m(\xi )=J^2_m\left( \xi \,c/2\right) \), then, we use Eq. (B1) along with appropriate trigonometric identities stated below
to get the following asymptotic expansions of \(M_n\) and \(X_m\)
Substituting Eqs. (B6) and (B7) in the equations \(N_n(\xi )=\xi \left[ M_n(\xi )-M_{n+1}(\xi )\right] \) and \(Y_m(\xi )=\xi \left[ X_m(\xi )-X_{m+2}(\xi )\right] \), respectively, yields
Calculation of \(\scriptstyle {\varphi _H}\) and \(\scriptstyle {\int _{0}^{\infty } \xi ^{-1}\,\varphi _H(\xi )\,J_1(\xi )\,\textrm{d}\xi }\)
In Table 8, we provide final expressions of \(\varphi _H\) and \(\int _{0}^{\infty } \xi ^{1}\,\varphi _H(\xi )\,J_1(\xi )\,\textrm{d}\xi \) corresponding to each case of heat flux loading.
Evaluation of \(\scriptstyle {I}\) and \(\scriptstyle {\partial I/\partial \zeta }\)
1.1 D.1 Case (a): uniform loading
In this case, we have \(I(\rho ,\zeta )=\int _{0}^{\infty } \xi ^{-1}\,\textrm{e}^{-\xi \left( \zeta +d\right) }\,J_0(\xi \,\rho )\,J_1(\xi )\,\textrm{d}\xi \).
For \(\zeta =-d\), using [45, Eqs. (6.574 1 and 2)], it yields
where F denotes the Gauss hypergeometric function defined by [45, Eq. (9.14)]
The relation (D1) can be simplified by expressing the Gauss hypergeometric function in terms of the complete elliptic integrals of the first and second kinds [45, p. 396]
In view of [45, Eqs. (9.137 13) and (9.131 1)], we have
Then, knowing from [45, Eqs. (8.114 1) and (8.113 1)] that
one obtains
For \(\rho =0\), we use [45, Eq. (6.623 3)] to get
Differentiating the previous equation with respect of \(\zeta \), we obtain
For \(\zeta >-d\) and \(\rho >0\), I and \(\partial I/\partial \zeta \) may be evaluated numerically.
1.2 D.2 Case (b): triangular loading
In this case, I and \(\partial I/\partial \zeta \) are calculated numerically.
1.3 D.3 Case (c): semi-elliptic loading
In this case, we have \(I(\rho ,\zeta )=\dfrac{3\,\sqrt{\pi }}{2\,\sqrt{2}}\displaystyle {\int _{0}^{\infty } \xi ^{-3/2}\,\textrm{e}^{-\xi \left( \zeta +d\right) }\,J_0(\xi \,\rho )\,J_{3/2}(\xi )\,\textrm{d}\xi }\).
For \(\zeta =-d\), using [45, Eqs. (6.574 1 and 2)], it yields
For \(\zeta >-d\), I and its derivative with respect to \(\zeta \) are calculated numerically.
1.4 D.4 Case (d): loading involving singularity
In this case, we have \(I(\rho ,\zeta )=\displaystyle {\dfrac{1}{2}\int _{0}^{\infty } \xi ^{-1}\,\textrm{e}^{-\xi \left( \zeta +d\right) }\,\sin (\xi )\,J_0(\xi \,\rho )\,\textrm{d}\xi }\).
For \(\zeta =-d\), using [45, Eq. (6.693 6)] and taking in to account that \(\textrm{arccosec}\,\rho =\arcsin (1/\rho )\), it yields
For \(\zeta >-d\), we use [45, Eq. (6.752 1)], to get
where \(\kappa ^\pm =\sqrt{\left( \rho \pm 1\right) ^2+\left( \zeta +d\right) ^2}\).
By differentiating Eq. (D14) with respect to \(\zeta \), we obtain
It is worth mentioning that, for \(\zeta >1-d\), we can alternatively evaluate I and \(\partial I/\partial \zeta \) in the first and third case by using [45, Eq. (6.626 1)].
Half-space medium subjected to a circular heat spot
The boundary conditions of a half-space heated by an arbitrary heat flux are given by Eqs. (11) and (16), where the superscripts (1) and (2) has been omitted here since the medium is continuous. Using the Hankel transform technique, the temperature expression satisfying the governing partial differential equation of this problem can be obtained as
where A is an unknown function to be determined. Thereafter, the temperature derivative with respect to \(\zeta \) is
Using the boundary condition (11) and Hankel transform theorem, we obtain
Substitution Eq. (E3) into Eq. (E1) leads to the following explicit formulas of the scaled temperature
where I is given by Eq. (38).
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Baka, Z., Kebli, B. Heat conduction problem for a half-space medium containing a penny-shaped crack. Arch Appl Mech 93, 635–662 (2023). https://doi.org/10.1007/s00419-022-02291-2
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DOI: https://doi.org/10.1007/s00419-022-02291-2