Abstract
Torsion of a cracked elastic body by an embedded semi-infinite rigid cylinder is studied. A coaxial penny-shaped crack is situated in the plane of the end of the cylinder. The problem is reduced to a system of dual integral equations including Hankel and Weber–Orr transforms and then, by using ansatzs, to an integral equation of the second kind with Hankel integral operator given on a semi-infinite interval or to an equivalent infinite system of linear algebraic equations with a Hankel matrix. A detailed investigation allowed us to suggest efficient methods for solving equations for any size of the crack. In particular, accurate approximate formulas for the stress intensity factor and the contact stresses are derived, as well as an asymptotic formula for the stress intensity factor when a crack is large. Analytical estimations and calculations manifest a strong increase in the stress intensity factor and the contact stress at the end of the cylinder as the crack tip is very close to the cylinder surface.
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1 Introduction
In this article, we consider static torsion of a cracked elastic space with the semi-infinite cavity \(r=a\), \(0\le z<\infty \), \(0\le \theta \le 2\pi \), and the coaxial crack \(z=0\), \(a\le r\le b\), \(0\le \theta \le 2\pi \), twisted by an embedded semi-infinite rigid circular cylinder whose cylindrical surface is bonded to the surface of the cavity and whose flat end is not in contact with the elastic medium. The cylinder is rotated through an angle \(\gamma \) about the axis z.
The problem stated above describes the leading asymptotic term for the torsional stress–strain state of a semi-infinite elastic body deformed by rotation of a partially embedded long rigid cylinder (a pin, a single rigid cylindrical pile or a rigid cylindrical pier) that has induced a crack. Our goal is to get an efficient approximate solution by basing on rigorous analytical methods and estimations of accuracy for approximations.
If a crack is absent, various torsional problems describing torsional stress in the vicinity of the base of a rigid or elastic inclusion were studied in [4, 5, 8, 18,19,20,21,22]. Note that the problem investigated in this article is a typical mixed boundary value problem, and therefore methods of the papers mentioned above cannot be applied in this case. Readers can find some mathematical similarity of the considered problem with the Reissner–Sagoci-type torsional contact problems for a half-space with a circular cylindrical hole or inclusion [1, 3, 15] and analogous axisymmetric contact problems [2, 11,12,13,14, 16].
In the dimensionless cylindrical coordinates \(\rho =r/a\), \(\theta \), \(\zeta =z/a\), the boundary conditions are:
where \(\beta =b/a>1\).
The only nonvanishing displacement \(u_{\theta }\left( \rho ,\zeta \right) \) obeys the partial differential equation (Lurie [9])
and the non-trivial components of the stress tensor are expressed via \( u_{\theta }\left( r,z\right) \) by the formulas
where G is the shear moduli.
The following integral representations in the form of inverse Hankel and Weber–Orr transforms (Titchmarsh [23]) with integrands including the Bessel functions \(J_{\nu }\left( \xi \right) \), \(Y_{\nu }\left( \xi \right) \) and \( H_{\nu }^{\left( 1\right) }\left( \xi \right) \),
satisfy the differential equation (6) and boundary condition (1). On inserting into the remaining boundary conditions (2),(3),(4) and (5), the above representations yield the system of the dual integral equations:
In Sect. 2, by using ansatzs and discontinuous integrals, the system of the dual integral equations is reduced to an Abel-type integral equation and, after that, to an integral equation of the second kind on the infinite interval \([\beta ,\infty )\) with an integral operator whose kernel depends on the sum of the arguments (a Hankel integral operator). This integral equation is shown to have in \(L^{2}\left( \beta ,\infty \right) \) a unique solution \(\omega \left( x\right) \) such that \(x\omega \left( x\right) \in C^{\infty }[\beta ,\infty )\cap L^{1}\left( \beta ,\infty \right) \) which provides a unique solution of the problem studied in the article.
In Sect. 3, the expressions in terms of \(\omega \left( x\right) \) for the stress intensity factor at the tip of the crack and the contact stress between the cylinder and elastic body are derived and certain lower bounds for the quantities mentioned above are obtained. In particular, the contact stress at the base of the cylinder is shown to be finite but large as the tip of the crack is very close to the cylinder surface.
Highly efficient analytic approximate formulas for \(\omega \left( x\right) \) and a quantities of interests, as well as estimates of their errors, are obtained in Sect. 4 as \(\beta \ge 1.01\) by basing on the little known in the research community formulas for approximate solutions of linear operator equations given in [10].
An approach for solving the integral equation, which is efficient also for small \(\beta -1\), is given in Sect. 5. The solution \(\omega \left( x\right) \) is represented in the form of an orthogonal series with coefficients to be a \(l_{1}\)-solution of an infinite system of linear algebraic equations whose matrix operator is a sum of the unit operator and a compact in \(l_{2}\) Hankel matrix operator. Truncating the infinite system to a finite system by using finite-dimensional operators with upper anti-triangular matrix as approximations for the Hankel operator, we first find an approximate \(l_{2}\)-solution which then is used to construct an approximate solution of the problem. The estimates of errors for approximate quantities of interest found in such a way are given. For very small \(\beta -1\), the order of finite systems is rather large. In this case, we suggest a novel highly efficient iterative procedure that allows us to get an approximate solution and estimate its error. The methods suggested in this section can be helpful in various problems of mechanics, mathematical physics and engineering.
Asymptotic formula for the stress intensity factor is derived in Sect. 6 for a large crack, \(\beta \ge 1.7\), by analyzing terms of the integral equation Neumann series with asymptotic evaluating arising integrals.
Results of calculations of the stress intensity factor and the contact stress are discussed in Sect. 7. Some estimates for solutions of integral equations that are exploited in the article are obtained in the “Appendix.”
2 Reducing the problem to an integral equation of the second kind
To solve the system of the dual integral equations obtained in the preceding section, we make use of the integrals
On evaluating the first integral [17] and rotating the path of integration in the second integral on the right side of (14) to \(90^{\circ }\),
where \(H\left( x\right) \) is the Heaviside unit step function and \(I_{\nu }\left( \xi \right) \ \)and \(K_{\nu }\left( \xi \right) \) are modified Bessel functions.
Represent \(A\left( \xi \right) \) and \(B\left( \xi \right) \) in the form of the ansatzs:
with \(\psi \left( t\right) \) to be determined.
Insert (18) and (20) into (10), (11) and (12). Interchanging the order of integration, we ascertain by exploiting (15) that the above ansatzs satisfy identically the above-said equations.
On inserting (17) and (19) into (13) and interchanging the order of integration, we obtain by exploiting (15) and (16):
where
The integral term on the left side of (21) is the well-known Abel integral operator [6]. Inverting the Abel operator and evaluating arising integrals
yields the integral equation of the second kind on semi-infinite interval
Expressing \(K_{3/2}\left( x\right) \) in terms of exponential function and integrating by parts, we have the estimate \(0<L\left( x,t\right) <\Theta \left( xt\right) ^{-1/2}\left( x+t\right) ^{-1}\), where \(\Theta \) is a constant. Then, \(\int \limits _{\beta }^{\infty }\int \limits _{\beta }^{\infty }L^{2}\left( x,s\right) dxds<\infty \), and therefore the self-adjoint integral operator \({\mathbf {L}}\) is a positive compact operator in the Hilbert space \(L^{2}\left( \beta ,\infty \right) \), which transforms functions from \(L^{2}\left( \beta ,\infty \right) \) into function belonging to \(L^{2}\left( \beta ,\infty \right) \cap C^{\infty }[\beta ,\infty )\). Hence, any \(L^{2}\left( \beta ,\infty \right) \)-solution \(\sqrt{x}\psi \left( x\right) \) belongs to \( L^{2}\left( \beta ,\infty \right) \cap C^{\infty }[\beta ,\infty )\) and can be written in the form
where \(s\omega ^{*}\left( s\right) \) is an integrable on \([\beta ,\infty )\) function.
By inserting (24) into (22), interchanging the order of integration and differentiating, we obtain the integral equation of the second kind:
in which \({\mathbf {R}}\) is a positive self-adjoint integral operator whose kernel is continuous on \([\beta ,\infty )\times [\beta ,\infty )\),
It is readily seen by using asymptotic expansions of Laplace integrals and behavior of cylindrical functions at \(\xi =0\) that \(R\left( x+s\right) =O\left( 1/\left( x+s\right) ^{3}\right) \) as \(x+s\rightarrow \infty \). Therefore, \({\mathbf {R}}\) is a positive compact operator in \(L^{2}\left( \beta ,\infty \right) \), and if \(\omega ^{*}\left( x\right) \) is a \( L^{2}\left( \beta ,\infty \right) \), then \(\omega ^{*}\left( x\right) \in C^{\infty }[\beta ,\infty )\cap L^{2}\left( \beta ,\infty \right) \). Also, the estimate \(\left| {\mathbf {R}}\omega ^{*}\left( x\right) \right| \le \left\| \omega ^{*}\left( s\right) \right\| _{L^{2}}\left\| R\left( x+s\right) \right\| _{L^{2}}\) involves \( x\omega ^{*}\left( x\right) \in C^{\infty }[\beta ,\infty )\cap L^{1}\left( \beta ,\infty \right) \). Since \(\mathbf {I+R}\) is a coercive operator, such a \(L^{2}\left( \beta ,\infty \right) \)-solution exists and is unique for any \(\beta >0\).
Now, note that \(\psi \left( \beta \right) \ne 0\). Otherwise, it follows from (25) that \(\omega ^{*}\left( x\right) =0\) and then (24) gives \(\psi \left( x\right) \equiv 0\). But the latter is impossible because \( \psi \left( x\right) =0\) does not satisfies (22).
Thus, one can write
and solve (28) instead of (22).
To determine the unknown constant \(\psi \left( \beta \right) \), one can note that (22) involves
Setting \(x=\infty \) in (24) yields
In conclusion of this section, we note that the aforementioned properties of \(\psi \left( x\right) \) and \(\omega \left( x\right) \) manifest that pertaining integrals in this section converge absolutely and uniformly. This validates all formal operations made in the process of deriving the above equations. Thus, there exists an unique solution of the problem if \(\omega \left( x\right) \) is a \(L^{2}\left( \beta ,\infty \right) \)-solution to (28). It will be seen in the next section that this solution also leads to physically correct results.
3 Stress intensity factor and contact stress
Once the function \(\psi \left( t\right) \) is determined, the stress on the crack plane \(z=0\), \(r\ge b\), is given by the relation:
Then, for \(r\in \left[ b,\infty \right] \),
where \(\psi \left( \beta \right) \) is given by (29).
Now, the stress intensity factor is given by the formula
Then, by using the estimate for \(\psi \left( \beta \right) \) obtained in the “Appendix,” we have the lower estimate
with
Thus, as it is expected, \(K_{III}\rightarrow \infty \) if \(\beta \rightarrow 1 \).
The contact stress \(\tau _{\theta r}\left( a,z\right) \), \(z\ge 0\), is evaluated by making use of (20), (24), (27), (29) and (15):
with
where the integral \(\Phi \left( x,\zeta \right) \) is transformed into the form (34) by rotating the path of integration to \(90^{\circ }\), \(\Phi \left( x,\zeta \right) \ =O\left( 1/x^{2}\right) \) as \(x\rightarrow \infty \), and \(\Phi \left( x,\zeta \right) \ =O\left( 1/z^{2}\right) \) as \( z\rightarrow \infty \). Note that \(k\left( \xi \right) =\exp \left( -\xi x\right) /\left( \xi K_{1}\left( \xi \right) \right) \) is a bounded monotonically decreasing function that tends to zero as \(\xi \rightarrow \infty \) and has a monotonically increasing negative derivative. Then, it is well known that the continuous function \(2x\Phi \left( x,\zeta \right) \), a cosine Fourier transform of \(k\left( \xi \right) \), is positive for \( 0\le \zeta \) \(\le \infty \).
At the point \(z=0\), the contact stress can be written as
According to the estimates given in the “Appendix,” \(\omega \left( x\right) \) and the denominator in the above formula are positive. Then, by noting \(\Phi \left( x,0\right) -\Phi \left( \beta ,0\right) <0\), one might see that all terms on the right side are negative, and therefore
Now, by rewriting \(\Phi \left( \beta ,0\right) \) in the form
where the integral converges absolutely and uniformly with respect to \(\beta \ge 1\), we infer that for very small \(\beta -1\) the contact stress \(\tau _{\theta r}\left( a,z\right) \) appears to be large at the end of the cylinder.
4 Approximate formulas for the stress intensity factor and contact stress
Because \({\mathbf {I}}+{\mathbf {R}}\) is a bounded coercive self-adjoint operator,
an efficient approximate \(L^{2}\)-solution to (28), \({\widetilde{\omega }}\left( x\right) \), can be found by the formulas suggested by Malits [10]:
where the polynomial \(P_{n}\left( x\right) \) is expressed in terms of the Chebyshev polynomials \(T_{n}\left( x\right) \):
and the error estimate is
The number \(\rho _{R}\) can be evaluated as the following:
Using the identity
we have as \( 0<\ \xi ,\upsilon <\infty \),
Finally, on inserting (39) and integrating term by term, we obtain
where
Integrating by parts shows that
In a similar manner, (38) involves
The values of \(\rho _{R}\) and \(\left\| R\left( x+s\right) \right\| _{L^{2}} \) versus \(\beta \) are given in Table 1.
An approximate solution \(\omega _{ap}\left( x\right) \in \) \(C^{\infty }[\beta ,\infty )\) can be determined by the formula
whose error is
Using the approximate solution (46) yields an approximate formula for \(\psi \left( \beta \right) \),
with
whose error estimate can be found by means of (36) and
The values of \(\left\| C\left( s,\beta \right) \right\| _{L^{2}}\) again can be found by using (38):
As given in Table 1, the simplest approximate inverse operator \( {\mathbf {A}}_{0}\ \) can be taken in a wide interval of the parameter \(\beta \). Then,
This leads to the approximate formula for the stress intensity factor at \( r=b \):
Evaluations show that a relative error of (52) monotonically decreases, is less than 1.45% as \(\beta \ge 1.01\), is less than 0.75% as \( \beta \ge 1.02\) and is less than 0.18% as \(\beta \ge 1.1\).
To derive an approximate formula for the contact stress at the end of the cylinder \(\tau _{\theta r}\left( a,0+\right) \), we take \(\omega \left( x\right) \approx {\widetilde{\omega }}\left( x\right) ={\mathbf {A}}_{0}R\left( x+\beta \right) \) and again exploit (38). Then,
with an error
Evaluations of the above coarse estimate manifest that a relative error of (53) monotonically decreases and is less than 1.06% as \(\beta \ge 1.01\), is less than 0.22% as \(\beta \ge 1.1\) and is less than 0.01% as \(\beta \ge 1.5\).
5 Reducing the problem to an infinite system of linear algebraic equations
The solution based on employing iterations of the integral operator suggested in the preceding section becomes inconvenient for very small \( \beta -1\) because of difficulties to ensure accurate calculating iterations as well as computing time which is needed. In this section, we will develop a more robust approach by reducing the integral equation to an infinite system of linear algebraic equations.
Let us represent a solution of the integral equation in the form of a series expansion in the orthonormal basis \(\{{\mathfrak {L}}_{m}\left( s\right) \}\),
where \(L_{m}\left( x\right) \) are Laguerre polynomials, and by exploiting the integral
expand \(R\left( x+s\right) \) into \({\mathfrak {L}}_{m}\left( x\right) \) series
where \(f_{m}\left( s\right) \) is defined by (44). The above series converges absolutely and uniformly on \([\beta ,\infty )\) because both \( \omega \left( x\right) \) and \(R\left( x+s\right) \) belong to \(C^{\infty }[\beta ,\infty )\cap L^{1}[\beta ,\infty )\).
Inserting (54) and (44) into (28), on integrating and equating coefficients of like elements of the basis \(\{{\mathfrak {L}} _{m}\left( x\right) \}\), we obtain an infinite system of algebraic equations:
where the matrix elements of the Hankel matrix operator \(c_{n+m}\) are given by (41) and \(f_{m}\left( \beta \right) \) by (44). Here, the operator \({\varvec{\Omega }}\), as a matrix representation of the operator \({\mathbf {R}}\), is compact in \(l_{2}\), positive and
Consequently, the operator \({\mathbf {I}}+{\varvec{\Omega }}\) is coercive: for \( \overrightarrow{z}\in l_{2}\),
and therefore (57) has in \(l_{2}\) a unique solution for any \(\beta >1\). By virtue of (45) and (42), a \(l_{2}\)-solution belongs to \(l_{1}\) also.
The compact matrix operator \({\varvec{\Omega }}\) can be approximated by some finite-dimensional operators \({\varvec{\Omega }}_{N}\) obtained with certain truncations of \({\varvec{\Omega }}\) under the condition that a sequence of operators \({\varvec{\Omega }}_{N}\) converges to \({\varvec{\Omega }}\) in \(l_{2}\) as \(N\rightarrow \infty \). We take the operators with upper anti-triangular matrices
as such operators. Then, \(\left\| {\varvec{\Omega }}_{N}\right\| _{l_{2}}\le \rho _{N}\),
and therefore \(\left\| {\varvec{\Omega }}-{\varvec{\Omega }}_{N}\right\| _{l_{2}}\rightarrow 0\) as \(N\rightarrow \infty \).
Thus, the approximation of coefficients \(\omega _{n}\) in \(l_{2}\) can be found by determining a vector \(\overrightarrow{\widetilde{\omega }}=( {\widetilde{\omega }}_{0},\widetilde{\omega }_{1},{\widetilde{\omega }}_{2},\ldots )\) from the system
The matrix operator \({\varvec{\Omega }}_{N}\) can be represented as a sum:
where the Hankel operator \(\widetilde{{\varvec{\Omega }}}_{N}\) is positive in \( l_{2}\) and in the Euclidean space \({\mathbb {R}}^{n}\), \(n\ge 2N+1\),
while
Now, it follows from
that the operator \({\mathbf {I}}+{\varvec{\Omega }}_{N}\) is coercive at least for sufficiently large N. In such a case, the system (60) has a unique solution.
To estimate an error of the approximate solution \(\overrightarrow{{\widetilde{\omega }}}\), we note that the equality
involves
Hence, due to (58)
and then by virtue of (59) the error estimate is
The series
will give \(L_{2}\) approximations of \(\omega \left( x\right) \). Hence, by using Parseval’s equation
Inserting the (63) series in (25) yields an accurate approximate solution in \(C[\beta ,\infty )\cap L^{1}\left( \beta ,\infty \right) \),
and then
Some additional simplification can be achieved by truncating infinite series in (64) and (65) by using (61).
When \(\beta -1\) is very small, evaluations show that matrix element \(c_{n+m}\) are decreasing very slowly and then \(\sqrt{\rho _{R}^{2}-\rho _{N}^{2}}\) becomes small only if 2N is rather large. For example, \(\sqrt{\rho _{R}^{2}-\rho _{200}^{2}}=0.0\,412\) for \(\beta =1.0004\). It is important in this situation that for evaluation of matrix elements of \({\varvec{\Omega }}_{N}\) one should evaluate \(2N+1\) integrals \( c_{0},c_{1},\ldots ,\) \(c_{2N}\) only. Another important point in such a case is that for achieving good accuracy it is preferable to solve a finite system of linear algebraic equation by some iterative algorithm which is rapidly convergent in \({\mathbb {R}}^{2N+1}\) norm. Taking into account that self-adjoint operator \({\varvec{\Omega }}_{N}\) might be chosen to be a coercive operator, one can again employ results of the paper by Malits [10] for constructing an iterative procedure. Then, an approximate solution has the form
where \(\overrightarrow{Z}=({\widetilde{\omega }}_{0},\widetilde{\omega } _{1},\ldots ,{\widetilde{\omega }}_{2N})\), \(\overrightarrow{F}=(f_{0},f_{1}, \ldots ,f_{2N})\) and the polynomial \(P_{n}\left( x\right) \) is defined by (35).
Using the recurrent formula for Chebyshev polynomials
one derives from (35)
Hence, we obtain the following iterative algorithm:
whose error estimate
is less than error estimates of other algorithms based on using (explicitly or implicitly) M iterations of operator \({\varvec{\Omega }}_{N}\) [10]. For \( N=200\) and \(\beta \ge 1.0004\), \(\varepsilon _{2}\le 0.003\,07\) and \(\varepsilon _{3}\le 0.00022\).
6 Stress intensity factor for a large crack.
The norms of the operator \({\mathbf {R}}\) in \(C[\beta ,\infty )\) and in \( L^{1}\left( \beta ,\infty \right) \) are given by the Laplace integral:
where \(q\left( \beta \right) \) is a monotonically decreasing function of the parameter \(\beta \), \(q\left( 1.0004\right) =0.985\). Then, the Neumann series
converges absolutely and uniformly for \(\beta \ge 1.0004\).
The inequality
involves that for \(\beta \ge 1.0004\) the terms of the Neumann series are alternating and monotonically decreasing in magnitude. For large \(\beta \):
The above estimates manifest that terms of the Neumann series constitute an asymptotic scale as \(\left( 2\beta \right) ^{2}\) is large and the Neumann series therefore is an asymptotic expansion. Hence, we find
where the asymptotic order of error is derived by using the estimates
Taking \(N=2\) and expanding Laplace integrals \(C\left( x,\beta \right) \) and \( R\left( s+x\right) \) into asymptotic series, we finally obtain
The approximate formula for the stress intensity factor
is asymptotically exact for large \(4\beta ^{2}\), and its relative error is a decreasing function of the parameter \(\beta \). For \(\beta =1.75\), the relative error is 3.4%, and for \(\beta =2.5\) the relative error is 0.5%.
7 Results
The results of calculations of the stress intensity factor are represented in Fig. 1, where the dotted line gives approximate values evaluated by the asymptotic formula (72). We observe a very rapid decrease in the stress intensity factor as the parameter \(\beta \) is increasing. This means that one can expect a state of the crack arrest for a sufficiently large \( \beta =b/a\). If the tip of the crack is very close to the end of the rigid cylinder, then the crack can be unstable.
The normalized contact stress \(T=\tau _{\theta r}\left( a,0+\right) /\gamma G \) is presented in Fig. 2. Despite the fact that the contact stress is finite for any \(\beta >1\), the contact stress is very large as the tip of the crack is very close to the end of the rigid cylinder. In the latter case, a debonding or damage zone can be developed at the end of the cylinder along the lateral surface.
8 Conclusions
We study torsion of an elastic space by an embedded semi-infinite rigid cylinder which has caused a coaxial penny-shaped crack in the plane of the cylinder end. The problem is reformulated as a system of dual integral equations containing inverse Bessel and Weber–Orr integral transforms. By using special ansatzs, the system of dual integral equations is reduced to solving an integral equation of the second kind with Hankel integral operator given on a semi-infinite interval. The stress intensity factor and contact stress are expressed in terms of a solution to the integral equation. A detailed investigation of the integral equation permits us to suggest accurate methods for its efficient solving for any size of the crack. In particular, approximate formulas for the contact stress at the end of the cylinder and stress intensity factor are derived. When the crack is large, an asymptotic formula for the stress intensity factor is obtained as well. Analytical estimations and calculations manifest a strong increase in the stress intensity factor and the contact stress at the end of the cylinder as the crack tip is very close to the cylinder surface.
References
Arutunyan, N.H., Abramyan, B.L.: Some axisymmetric problems for a half-space and an elastic layer with a vertical cylindrical notch. J. Izv. AN Arm. SSR. Mek. 22, 3–13 (1969). In Russian
Bandyopadhyay, K.K., Kassir, M.K.: Contact problems for solids containing cavities. J. Eng. Mech. ASCE 104, 1389–1402 (1978)
Dhaliwal, R.S., Singh, B.M., Sneddon, I.N.: A problem of Reissner–Sagoci type for an elastic cylinder embedded in an elastic half-space. Int. J. Eng. Sci. 17, 139–144 (1979)
Hasegawa, H., Ichikawa, F.: Torsion of an elastic solid cylinder embedded in an elastic half space. Trans. Jpn. Soc. Mech. Eng. A. 64, 650–655 (1998)
Karasudhi, P., Rajapakse, R.K.N.D., Hwang, B.Y.: Torsion of a long cylindrical elastic bar partially embedded in a layered elastic half space. Int. J. Solids Struct. 20, 1–11 (1984)
Kilbas, A., Srivastava, H.M., Trujillo, J.J.: Theory and Applications of Fractional Differential Equations. North-Holland Mathematical Studies. Elsevier, Amsterdam (2006)
Krasnoselskii, M.A., Vainikko, G.M., Zabreiko, P.P., Ruticki, Y.B., Stet’senko, V.Y.: Approximate Solution of Operator Equations. Wolters-Noordhoff Publications, Groningen (1972)
Luko, J.E.: Torsion of a rigid cylinder embedded in an elastic half-space. J. Appl. Mech. 43, 419–423 (1976)
Lurie, A.I.: Theory of Elasticity. Springer, Berlin (2005)
Malits, P.: Certain approximative methods for solving linear operator equations. Appl. Math. Lett. 20, 306–311 (2007)
Malits, P.Y.: A contact problem for a half-space with a rigid supporting surface at a cylindrical hole. Dinamicheskie Sistemy 3, 39–44 (1984). (in Russian)
Malits, P.Y.: An axially symmetric contact problem for a half-space with an elastically reinforced cylindrical cavity. J. Sov. Math. 57, 3417–3420 (1991)
Malits, P.Y., Privarnikov, A.K.: Effect of a punch on a half-space with a circular cylindrical hole. In: Problems of Strength and Plasticity, pp. 137–151. Dniepropetrovsk University, Dniepropetrovsk (1971) (in Russian)
Malits, P.Y., Snitser, A.R.: Vertical oscillations of a circular die on an elastic half-space with a cylindrical cavity. J. Sov. Math. 65, 1629–1634 (1993)
Malits, P.Y., Snitser, A.R., Shevlyakov, Y.A.: Solution of the Reissner–Sagoci problem for a half-space with a cylindrical cavity. Int. Appl. Mech. 25, 24–30 (1989)
Parlas, S.C., Michalopoulos, C.D.: Axisymmetric contact problem for an elastic half-space with a cylindrical hole. Int. J. Eng. Sci. 10, 699–707 (1972)
Prudnikov, A.P., Brychkov, Y.A., Marichev, O.I.: Integrals and Series, V. 2. Scripta Technica Inc., Gordon and Breach Science Publishers, New York (1987)
Rajapakse, R.K.N.D.: A torsion load transfer problem for a class of non-homogeneous elastic solids. Int. J. Solids Struct. 24, 139–151 (1988)
Rajapakse, R.K.N.D., Selvadurai, A.P.S.: Torsional stiffness of non-uniform and hollow rigid piers embedded in isotropic elastic media. Int. J. Numer. Anal. Methods Geomech. 9, 525–539 (1985)
Selvadurai, A.P.S.: On the torsional stiffness of rigid piers embedded in isotropic elastic soils. In: Langer, J., Mosley, E., Thompson, C. (eds.) Laterally Loaded Deep Foundations: Analysis and Performance, pp. 49–55. ASTM International, West Conshohocken (1984)
Selvadurai, A.P.S., Rajapakse, R.K.N.D.: A variational scheme for the analysis of torsion of nonuniform elastic bars embedded in elastic media. J. Eng. Mech. ASCE 113, 1534–1550 (1987)
Tian-qua, Y.: Torsion of rigid circular shaft of varying diameter embedded in an elastic half space. Appl. Math. Mech. 9, 449–453 (1988)
Titchmarsh, E.C.: Eigenfunction Expansions Associated with Second Order Differential Equations. Oxford University Press, Oxford (1962)
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Appendix: Some estimates for \(\omega \left( x\right) \) and \( \psi \left( b\right) \)
Appendix: Some estimates for \(\omega \left( x\right) \) and \( \psi \left( b\right) \)
Let us rewrite (28) in the form
where the self-adjoint operator \(\left( 1-\mu \right) {\mathbf {I}}-\mu {\mathbf {R}}\) is positive. According to [7], there exists a \(L^{2}\)-solution of the above equation that is a limit of the successive approximations
and consequently this solution is positive and, as it shown in Sect. 2, unique,
We have from (28)
Then, on integrating
where \(C\left( \beta \right) \) is defined by (31).
Now, (29) involves
Note that \(C\left( \beta \right) \) is a monotonically decreasing function of the parameter \(\beta \) and \(C\left( 1\right) =\infty \).
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Malits, P. Torsion of a cracked elastic body by an embedded semi-infinite rigid cylinder. Z. Angew. Math. Phys. 71, 35 (2020). https://doi.org/10.1007/s00033-020-1255-3
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DOI: https://doi.org/10.1007/s00033-020-1255-3
Keywords
- Elasticity
- Crack
- Stress intensity factor
- Contact
- Integral equations
- Approximate solution
- Infinite system of algebraic equations
- Iterative solving system of algebraic equations