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Matrix stiffness

Therefore the assembled global stiffness matrix in this case is written as... [Pg.49]

Note that the definite integrals in the members of the elemental stiffness matrix in Equation (2.77) are given, uniformly, between the limits of -1 and +1. This provides an important facility for the evaluation of the members of the elemental matrices in finite element computations by a systematic numerical integration procedure (see Section 1.8). [Pg.53]

The momentum and continuity equations give rise to a 22 x 22 elemental stiffness matrix as is shown by Equation (3.31). In Equation (3.31) the subscripts I and / represent the nodes in the bi-quadratic element for velocity and K and L the four corner nodes of the corresponding bi-linear interpolation for the pressure. The weight functions. Nr and Mf, are bi-qiiadratic and bi-linear, respectively. The y th component of velocity at node J is shown as iPj. Summation convention on repeated indices is assumed. The discretization of the continuity and momentum equations is hence based on the U--V- P scheme in conjunction with a Taylor-Hood element to satisfy the BB condition. [Pg.84]

FLOW. Calculates members of the elemental stiffness matrix corresponding to the flow model. [Pg.211]

Step 1 To solve a Stokes flow problem by this program the inertia term in the elemental stiffness matrix should be eliminated. Multiplication of the density variable by zero enforces this conversion (this variable is identified in the program listing). [Pg.215]

COMPUTER SIMULATIONS - FINITE ELEMENT PROGRAM Stiffness matrix corresponding to flow equations in (x, 3O formulation... [Pg.216]

Step 3 Comparing systems (7.2) and (7.3) additional terms in the members of the stiffness matrix corresponding to the axisymmetric fon-nulation are identified. Note that the measure of integration in these tenns is (r drdz). [Pg.216]

After evaluation of the terms of the stiffness matrix modify them according to the additional tenns shown in system (7.3). [Pg.217]

C ASSEMBLE GLOBAL STIFFNESS MATRIX IN A BANDED FORM C... [Pg.240]

SOLVES THE GT,OBAL STIFFNESS MATRIX USING LU DECOMPOSITION... [Pg.241]

Stiffness Matrix Method. The stiffness method can be expressed in matrix form as follows ... [Pg.62]

In contrast to the flexibiUty method, the stiffness method considers the displacements as unknown quantities in constmcting the overall stiffness matrix (K). The force vector T is first calculated for each load case, then equation 20 is solved for the displacement D. Thermal effects, deadweight, and support displacement loads are converted to an equivalent force vector in T. Internal pipe forces and stresses are then calculated by applying the displacement vector [D] to the individual element stiffness matrices. [Pg.63]

The most recent developments in computational stmctural analysis are almost all based on the direct stiffness matrix method. As a result, piping stress computer programs such as SIMPLEX, ADLPIPE, NUPIPE, PIPESD, and CAESAR, to name a few, use the stiffness method. [Pg.63]

Calculate the stresses in the local directions using the on-axis stiffness matrix [Q] derived earlier. [Pg.186]

For the situation where the loading is applied off the fibre axis, then the above approach involving the Plate Constitutive Equations can be used but it is necessary to use the transformed stiffness matrix terms Q. [Pg.198]

A] is the Extensional Stiffness Matrix although it should be noted that it also contains shear terms. [Pg.205]

Thus the stiffness matrix for a symmetric laminate may be obtained by adding, in proportion to the ply thickness, the corresponding terms in the stiffness matrix for each of the plies. [Pg.205]

Having obtained all the terms for the extensional stiffness matrix [A], this may then be inverted to give the compliance matrix [a]. [Pg.205]

The Stiffness matrix [Q] is obtained as earlier each individual ply in the laminate. [Pg.206]

The Stiffness matrix [A] for the laminate is determined by adding the product of thickness and [Q for each ply. [Pg.206]

Mechanical Behaviour of Composites Overall Stiffness Matrix Q(0) = T- Q T,... [Pg.207]

This is called the Extensional Stiffness Matrix and the similarity with that derived earlier for the single ply should be noted. [Pg.209]

Overall Stiffness Matrix Overall Compliance Matrix... [Pg.471]

The Extension Stiffness Matrix is then obtained from... [Pg.471]


See other pages where Matrix stiffness is mentioned: [Pg.43]    [Pg.75]    [Pg.76]    [Pg.220]    [Pg.221]    [Pg.232]    [Pg.233]    [Pg.239]    [Pg.63]    [Pg.67]    [Pg.86]    [Pg.12]    [Pg.13]    [Pg.184]    [Pg.186]    [Pg.187]    [Pg.189]    [Pg.197]    [Pg.206]    [Pg.207]    [Pg.219]    [Pg.470]    [Pg.472]    [Pg.472]   
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See also in sourсe #XX -- [ Pg.184 ]




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Bending stiffness matrix

Coupling stiffness matrix

Element stiffness matrix

Extensional stiffness matrix

Flexural stiffness matrix

Global stiffness matrix

In-plane stiffness matrix

Linear stiffness matrix

Matrix stiffness tensor

Stiff Stiffness

Stiffness

Stiffness coefficient matrix

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