Download PDF by Andreas Öchsner: Computational Statics and Dynamics: An Introduction Based on

By Andreas Öchsner

ISBN-10: 9811007322

ISBN-13: 9789811007323

ISBN-10: 9811007330

ISBN-13: 9789811007330

This booklet introduces readers to fashionable computational mechanics in accordance with the finite point strategy. It is helping scholars reach mechanics classes via exhibiting them tips on how to follow the basic wisdom they received within the first years in their engineering schooling to extra complicated topics.

In order to deepen readers’ realizing of the derived equations and theories, each one bankruptcy additionally comprises supplementary difficulties. those difficulties begin with primary wisdom questions about the idea provided within the bankruptcy, via calculation difficulties. In overall over eighty such calculation difficulties are supplied, besides short recommendations for each.

This booklet is principally designed to fulfill the desires of Australian scholars, reviewing the math coated of their first years at college. The 13-week direction includes 3 hours of lectures and hours of tutorials consistent with week.

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Extra info for Computational Statics and Dynamics: An Introduction Based on the Finite Element Method

Sample text

The first one modifies the system shown in Eq. 3 Finite Element Solution 41 where the last equation gives immediately the boundary condition as u 4X = u 0 . The solution of the system of equations given in Eq. 113) can be obtained by inverting the coefficient matrix and multiplying it with the vector on the right-hand side as: ⎤ ⎡1 ⎤ ⎡ u u 2X 3 0 ⎣u 3X ⎦ = ⎣ 2 u 0 ⎦ . 101) In general we can state that a non-homogeneous Dirichlet boundary condition at node n can be introduced in the system of equations by modifying the nth line in such a way that at the position of the nth column a ‘1’ is obtained while all other entries of the nth line are set to zero.

46 2 Rods and Trusses (a) (b) Fig. 16 Free body diagram of the cantilevered rod structure shown in Fig. 14 Based on the indicated reaction forces, the global (non-reduced) system of equations can be stated for the configuration in Fig. 128) L ⎣ 0 −1 2 −1 ⎦ ⎣u 3X ⎦ ⎣ 0 ⎦ u 4X F0 0 0 −1 1 or for Fig. 16b as: ⎤ ⎡ ⎤ ⎤⎡ −R1 1 −1 0 0 u 1X E A ⎢ −1 2 −1 0 ⎥ ⎢u 2X ⎥ ⎢ 0 ⎥ ⎥=⎢ ⎥. 129) Knowing all nodal displacements, the support reaction R1 can be obtained for both cases by evaluating the first equation of the linear system as: R1 = − EA (u 1X − u 2X ) .

1 Derivation of the Principal Finite Element Equation Let us consider in the following the governing differential equation according to Eq. 14). 15) EA dx 2 where u 0 (x) represents the exact solution of the problem. The last equation which contains the exact solution of the problem is fulfilled at each location x of the rod and is called the strong formulation of the problem. Replacing the exact solution in Eq. 15) by an approximate solution u(x), a residual r is obtained: r (x) = E A d2 u(x) + p(x) = 0.

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Computational Statics and Dynamics: An Introduction Based on the Finite Element Method by Andreas Öchsner


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