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MAT3

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Bulk Data Entry

MAT3 – Material Property Definition, Form 3

Description

Defines the material properties for linear, temperature-independent, and orthotropic materials used by the CTAXI and CTRIAX6 axisymmetric elements.

Format

(1)

(2)

(3)

(4)

(5)

(6)

(7)

(8)

(9)

(10)

MAT3

MID

EX

ETH

EZ

NUXTH

NUTHZ

NUZX

RHO

 

 

 

 

GZX

AX

ATH

AZ

TREF

GE

 

hmtoggle_plus1Example

(1)

(2)

(3)

(4)

(5)

(6)

(7)

(8)

(9)

(10)

MAT3

17

3.0+7

3.1+7

3.2+7

0.33

0.28

0.30

2.0e-5

 

 

 

 

7.0+6

1.1e-4

1.1e-4

1.2e-4

35.5

0.19

 

Field

Contents

MID

Unique material identification number.

No default (Integer > 0)

EX, ETH, EZ

Young’s Moduli in the x, θ and z directions, respectively.

No default (Real > 0.0)

NUXTH,
NUTHZ,
NUZX

Poisson’s Ratios:

NUXTH = Poisson’s Ratio for strain in the θ direction, when stress in the x direction.
NUTHZ = Poisson’s Ratio for strain in the z direction, when stress in the θ direction.
NUZX = Poisson’s Ratio for strain in the x direction, when stress in the z direction.

No default (Real)

RHO

Mass density.

No default (Real)

GZX

Shear Modulus in the x-z plane.

No default (Real > 0.0)

AX, ATH, AZ

Thermal expansion coefficient in the x, θ, and z directions, respectively.

No default (Real)

TREF

Reference temperature for thermal loading.

Default = blank (Real or blank)

GE

Structural element damping coefficient. See comment 6.

No default (Real)

Comments

1.The material identification number must be unique for all MAT1, MAT2, MAT8 and MAT9 entries.
2.Values of all seven elastic constants, EX, ETH, EZ, NUXTH, NUTHZ, NUZX and GZX must be present.
3.A warning is issued if absolute value of NUXTH or NUTHZ is greater than 1.0.
4.The x, θ and z directions are principal material directions of the material coordinate system. Each element (that is a CTAXI or CTRIAX6 element) supporting the use of MAT3 contains a “Theta” field to relate the principal material directions to the basic coordinate system.
5.The strain-stress relationship is:

mat3_strain-stress

Note that the strain and stress here are both defined in the material coordinate system.

6.To obtain the damping coefficient GE, multiply the critical damping ratio, C/C0, by 2.0.
7.This card is represented as a material in HyperMesh.

See Also:

Material Property Checks for MAT3

Bulk Data Section

Guidelines for Bulk Data Entries

Bulk Data Entries by Function

The Input File