13.290. ELBOW290 - 3-D 3-Node Elbow

Matrix or Vector Shape Functions Integration Points
Stiffness and Stress Stiffness Matrices; and Thermal and Newton-Raphson Load VectorsEquation 11–19, Equation 11–20, Equation 11–21, Equation 11–22, Equation 11–23, and Equation 11–24

Around the circumference: Fourier Series

Along the length:  2
Around the 
circumference: 8 or higher
Thru-the-thickness: 
 1, 3, 5, 7, or 9 per layer

Mass Matrix and Pressure Load Vector Same as stiffness matrix

Along the length:  3
Around the 
circumference: 8 or higher
Thru-the-thickness: 
 1, 3, 5, 7, or 9 per layer 

Load Type Distribution
Element Temperature

KEYOPT(1) = 0 Linear thru wall and linear along length

KEYOPT(1) = 1 Bilinear across cross-section and linear along length

Nodal Temperature Constant across cross-section, linear along length
Internal and External Pressures Constant

References:

Bathe and Almeida ([370])

Yan, Jospin, and Nguyen ([371])

13.290.1. Other Applicable Sections

Structures describes the derivation of structural element matrices and load vectors as well as stress evaluations.

13.290.2. Assumptions and Restrictions

Pipe cross-sectional motions (i.e., radial expansion, ovalization, and warping) are modeled with Fourier series. The corresponding unknowns (Fourier magnitudes) are treated as internal degrees of freedom. A higher number of Fourier modes may be required to achieve an adequate level of accuracy in cross-sectional motions. Also, a higher number of integration points around the circumference may be needed for capturing nonlinear material behaviors or ensuring sufficient numerical integration accuracy.

No slippage is assumed between the element layers. Shear deflections are included in the element; however, normals to the center wall surface are assumed to remain straight after deformation, but not necessarily normal to the center surface. Therefore, constant transverse shears through the pipe wall are allowed.

13.290.3. Shear Correction

The element uses an equivalent energy method to compute shear correction factors. These factors are predetermined based on the section lay-up at the start of solution


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