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panels 0.15.0 documentation

Plates and cylindrical shells
Bardell’s hierarchical functions
Boundary conditions
Loads
Multi-domain assemblies

Plates and cylindrical shells
Bardell’s hierarchical functions
Boundary conditions
Loads
Multi-domain assemblies
Stiffened panels
Panel flutter with the piston theory
Field outputs, plots and files
Follower pressure loads: theory
Large rotations: plates with Green-Lagrange membrane strains
Large rotations: total-Lagrangian Kirchhoff-Love plates
Third-order shear deformation theory with a laminate offset
Exact connections with the null-space method
Tangent stiffness matrix and its product by a vector
Approximation functions tabulated at the integration points
Cohesive zone model of the multi-domain approach
Linear static analysis
Linear buckling analysis
Frequency analysis
Panel flutter analysis
Non-linear static analysis with the Newton-Raphson method
Non-linear static analysis with the arc-length methods
Follower (hydrostatic) pressure
Prescribed displacements
Clamped and face-clamped edges
Cylinders modeled as multi-domain assemblies
Panels with a T-stiffener modeled as multi-domain assemblies
Wing-box modeled as a multi-domain assembly
Stiffened panel bays
API reference
Changelog
References

Section Navigation

Plates and cylindrical shells (panels.shell)
External force vector (panels.shell_fext)
Contour plots (panels.plot_shell)
Model database (panels.modelDB)
Bardell’s functions (panels.bardell)
Multi-domain assemblies (panels.multidomain)
Cylinders modeled as multi-domain assemblies
Panels with a T-stiffener modeled as 2D domains
Wing-box modeled as a multi-domain assembly
Blade stiffeners (panels.stiffener)
Stiffened panel bays (panels.stiffpanelbay)
Saving and loading in a JSON + NumPy zip container (panels.json_io)
Development tools (panels.dev)

API reference
Wing-box modeled as a multi-domain assembly

Wing-box modeled as a multi-domain assembly#

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Panels with a T-stiffener modeled as 2D domains

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Blade stiffeners (panels.stiffener)

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