Users:General FEM Analysis/Elements Reference/Shell NURBS KL
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(Difference between revisions)
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== General Description == | == General Description == | ||
− | This element is based on the [https://mediatum.ub.tum.de/node?id=1002634 Phd Thesis of J.Kiendl] | + | This element is based on the [https://mediatum.ub.tum.de/node?id=1002634 Phd Thesis of J.Kiendl]. |
=== Example of a Complete Input Block === | === Example of a Complete Input Block === | ||
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=== Element Type === | === Element Type === | ||
− | * | + | * The element formulation is well tested for static and dynamic linear and nonlinear analysis. |
− | * | + | * Stresses for nonlinear case need to be corrected. |
− | * | + | * Can be used for thin shell structures |
=== Degrees of Freedom === | === Degrees of Freedom === | ||
− | The element uses three translatoric degrees of freedom (''Disp_X'', ''Disp_Y'', ''Disp_Z'') | + | The element uses three translatoric degrees of freedom (''Disp_X'', ''Disp_Y'', ''Disp_Z'') at each control point. |
=== Parameter Description === | === Parameter Description === |
Revision as of 06:19, 9 December 2016
Contents |
General Description
This element is based on the Phd Thesis of J.Kiendl.
Example of a Complete Input Block
EL-PROP 1 : SHELL_NURBS_KL MAT= EL-MAT 1 !material property THICKNESS = 1.0 COUPLING = EL-PROP 6 !BRep coupling element to handle C^0 continuity inside the patch ! STABILIZATION = EL-PROP 7 !Stabilization element for improving condition number NEJA = NURBS !DIP or FULL !Method for handling the integration for trimmed elements(use NURBS) INT_TYPE_SHELL_NURBS_KL = USER !or FULL or OPTIMAL !FULL means p+1 and q+1;OPTIML uses in the interior of the patch less quadrature points (some tests required for higher polynomial degrees >3 ! GAUSS_U = 4 !# of quadratur points in u-dir in case of INT_TYPE = USER ! GAUSS_V = 4 !# of quadratur points in u-dir in case of INT_TYPE = USER
Element Type
- The element formulation is well tested for static and dynamic linear and nonlinear analysis.
- Stresses for nonlinear case need to be corrected.
- Can be used for thin shell structures
Degrees of Freedom
The element uses three translatoric degrees of freedom (Disp_X, Disp_Y, Disp_Z) at each control point.
Parameter Description
Compulsory Parameters | ||
Parameter | Values, Default(*) | Description |
---|---|---|
MAT | EL-MAT int | Linking to a material input block |
INT_TYPE_BEAM_3D_NURBS_KLRod | FULL, USER | Control of integration type.
|
CROSS SECTION | DIAMETER = float | circular cross section defined ba the diameter. A = d^2π/4, Iy = Iz = d^4π/32, It= d^4π/32 |
HEIGHT = float WIDTH = float |
rectangular cross section defined by height and width. A = h*w, Iy = h^3*w/12 Iz = h*w^3/12 It= min(h,w)^3*max(h,w)/3 | |
AREA = float IY = float IZ = float IT = float |
cross section defined directly | |
AXIS | AXIS float1 float2 float3 float4 | Definition of the cross sectional principal axis. Second axis is perpendicual to first and tangent of the curve. float1 is the position on the curve and float - float4 the direction (x,y,z). Base vectors are normalized and linearly interpolated for postions inbetween the defined ones. Axes for start and end knot of the NURBS curve are mandatory. |
Optional Parameters | ||
Parameter | Values, Default(*) | Description |
GAUSS_U | GAUSS_U = int | Number of Gauss point per element. Must only to be defined when INT_TYPE_BEAM_3D_NURBS_KLRod = USER |
Example of a Complete Input Block
EL-PROP 1 : BEAM_3D_NURBS_KLRod MAT= EL-MAT 1 DIAMETER=1.0 !or: HEIGHT=1.0 WIDTH=1.0 or: AREA=1.0000e+008 IY=1.0000e+008 IZ=1.0000e+008 IT=1.0000e+008 INT_TYPE_BEAM_3D_NURBS_KLRod = FULL !or: INT_TYPE_BEAM_3D_NURBS_KLRod = USER GAUSS_U = 3 ! U n1 n2 n3 AXIS 0.000000e+000 0.000000e+000 1.000000e+000 0.000000e+000 AXIS 1.000000e+000 0.000000e+000 1.000000e+000 0.000000e+000
Element Loading
The Beam_3D_NURBS_KLRod element is able to carry the following loads:
- dead load
- snow load
- pressure load
- moment
Benchmarks
The main benchmark file in the Carat++-repository is
- '../examples/benchmark_examples/isogeometric/iga_kl_rod_nln/cbm_iga_kl_rod_nln.txt'.
It is further used in:
- '../examples/benchmark_examples/isogeometric/iga_formfinding_4point_with_trusses/cbm_4PointSailwTrusses.txt'
References
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