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OCTOBER 19-20, 2012 - YMCA University of Science & Technology

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Proceedings <strong>of</strong> the National Conference on<br />

Trends and Advances in Mechanical Engineering,<br />

<strong>YMCA</strong> <strong>University</strong> <strong>of</strong> <strong>Science</strong> & <strong>Technology</strong>, Faridabad, Haryana, Oct <strong>19</strong>-<strong>20</strong>, <strong>20</strong>12<br />

ν<br />

⎡ 1<br />

0<br />

1 − ν<br />

⎤<br />

⎢ ν<br />

⎥<br />

1 − ν ⎢ 1 0 ⎥<br />

D =<br />

(1 + ν)(1 − 2ν) ⎢1 − ν<br />

⎥ Eq. (3)<br />

⎢<br />

(1 − 2ν)<br />

0 0<br />

⎥<br />

⎢<br />

2(1 − ν) ⎥<br />

⎣<br />

⎦<br />

When the closed crack splits, ∆u 1 (∆a — r, t) and∆u 2 (∆a — r, t) represents, respectively the crack sliding and<br />

opening displacement components at t with the following form [8]:<br />

∆u 1(∆a — r, t) = u 1 (∆a − r, π, t) − u 1 (∆a − r, −π, t)<br />

Eq. (4)<br />

∆u 2 (∆a — r, t) = u 2 (∆a − r, π, t) − u 2 (∆a − r, −π, t)<br />

Where ∆a is the virtual extended length <strong>of</strong> the crack and r is the radial crack length.<br />

3. Numerical Example<br />

In order to validate the effectiveness and accuracy <strong>of</strong> the current method for a cracked linear viscoelastic body, a<br />

fracture example is studied and numerical results are compared to available reference solutions. For the<br />

following example the material is assumed to be a three-parameter linear viscoelastic solid as shown in Figure 1.<br />

Two groups <strong>of</strong> assumed material properties are used in the validation case studies shown in Table 1.<br />

A viscoelastic strip having an edge crack with remotely applied tension as shown in Figure 2 is investigated. The<br />

height <strong>of</strong> strip is H=4W, where W=1 is the width <strong>of</strong> the strip. The crack depth is a=0.3W. Poisson’s ratio ν=0.49.<br />

The unit step loading is applied and the total loading time is T=<strong>20</strong>0. COD {u 2 (r, π, t)—u 2 (r,—π, t)}is computed<br />

at a pair <strong>of</strong> reference points A and B as shown in Figure 3.<br />

The formulation <strong>of</strong> displacement field at crack tip under remotely applied tension is [8]<br />

u 2 (r, θ, t) = Fσ 0 √πa(1 + ν) r<br />

k + 1 − 2π 2cos2 θ sin θ J(t)Eq. (5)<br />

2 2<br />

where u 2 is the y-direction displacement component in Cartesian coordinate system located at crack tip. r and θ<br />

are the polar coordinates defined around the crack tip. F is a nondimensional<br />

coefficient for stress intensity factor with the value 1.6599, J (t) is the creep compliance, and k<br />

is the Kolosov constant takes the value <strong>of</strong> k= (3- 4ν) for plain strain state andσ0 is assumed to be 1 [8].<br />

TABLE I<br />

MATERIAL PARAMETERS OF THE LINEAR VISCOELASTIC SOLID.<br />

Set E ∞ E 1 η 1<br />

A 1.0 1.0 5.0<br />

B 1.0 2.0 5.0<br />

Figure 1: The three-parameter linear viscoelastic solid.<br />

496

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