*MAT_026 (HONEYCOMB)
LS-DYNA Input Interface KeywordThis keyword defines an orthotropic compressible honeycomb material.
Format
(1) | (2) | (3) | (4) | (5) | (6) | (7) | (8) |
---|---|---|---|---|---|---|---|
*MAT_026 or *MAT_HONEYCOMB | |||||||
mat_ID | |||||||
LC1 | LC2 | LC3 | LCS | LC12 | LC23 | LC31 | LCSR |
EAAU | EBBU | ECCU | GABU | GBCU | GCAU | AOPT | |
A1 | A2 | A3 | |||||
D1 | D2 | D3 | TSEF | SSEF |
Definition
Field | Contents | SI Unit Example |
---|---|---|
mat_ID | Material identifier. (Integer) |
|
Initial density. (Real) |
||
LC1 | Stress versus either relative volume or volumetric strain in
direction 1. (Real) |
|
LC2 | Stress versus either relative volume or volumetric strain in
direction 2. (Real) |
|
LC3 | Stress versus either relative volume or volumetric strain in
direction 3. (Real) |
|
LCS | Shear stress versus either relative volume or volumetric
strain. (Real) |
|
LC12 | Shear stress versus shear strain in direction
12. (Real) |
|
LC23 | Shear stress versus shear strain in direction
23. (Real) |
|
LC31 | Shear stress versus shear strain in direction
31. (Real) |
|
LCSR | Scaling coefficients for stress versus strain
rate. (Real) |
|
LC31 | Shear stress versus either relative volume or volumetric
strain in direction 31. (Real) |
|
E11 | Young's modulus in direction 1. (Real) |
|
E11 | Young's modulus in direction 2. (Real) |
|
E11 | Young's modulus in direction 3 (Real) |
|
G12 | Shear modulus in direction 12. (Real) |
|
G23 | Shear modulus in direction 23. (Real) |
|
G32 | Shear modulus in direction 32. (Real) |
|
AOPT | Orthotropy axis option.
(Integer) |
|
A1, A2, A3 | First orthotropy direction vector for
AOPT=2. (Real) |
|
D1, D2, D3 | With A1, A2,
A3 determines 12 plane of orthotropy for
AOPT=2. (Real) |
|
TSEF | Tensile strain to failure. (Real) |
|
SSEF | Shear strain to failure. (Real) |
Comments
- This material law maps to /MAT/LAW50 (VISC_HONEY) and /PROP/TYPE6 (SOL_ORTH).
- The material is fully compressible. All degrees of freedom are decoupled.
- Curves in directions 1, 2, 3 are engineering stresses as functions of either volumetric strain, which means the first abscissa point is negative or relative volume (the first abscissa point is positive).
- Positive stresses and strains correspond to compression in direction 1, 2, 3.
- The option “_TITLE” can be added to the end of this keyword. When “_TITLE” is included, an extra 80 characters long line is added after the keyword input line which allows an entity title to be defined.