1.4.9 Coupled temperature-displacement elements

Products: ABAQUS/Standard ABAQUS/Explicit

I. Coupled temperature-displacement truss elements

Problem description

Model:

Length	7.0
Area	3.0
Centrifugal axis of rotation	(0, 1, 0) through origin
Coriolis axis of rotation	(0, 0, 1) through origin (2-D)
	(0, 1, 0) through origin (3-D)
Gravity load vector	(0, –1, 0)

Material:

Young's modulus	30 × 10⁶
Coefficient of thermal expansion	0.0
Thermal conductivity	3.77 × 10^–5
Density	82.9
Sink (bulk fluid) temperature	75.0
Absolute zero temperature	–460.0

Initial conditions:

Initial velocity	ALL, 1, 5.0
	ALL, 2, 2.0

Results and discussion

The calculated reactions are in agreement with the applied loads.

Input files

T2D2T element load tests:

et22tfdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, R1, R2, S1, S2.

et22tfdr.inp

ROTA.

T2D3T element load tests:

et23tfdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, R1, R2, S1, S2.

et23tfdr.inp

ROTA.

T3D2T element load tests:

et32tfdd.inp

BX, BY,BZ, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, R1, R2, S1, S2.

et32tfdd_po.inp

*POST OUTPUT analysis.

et32tfdr.inp

ROTA.

T3D3T element load tests:

et33tfdd.inp

BX, BY, BZ, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, R1, R2, S1, S2.

et33tfdr.inp

ROTA.

II. Coupled temperature-displacement plane stress, plane strain and generalized plane strain elements

Problem description

Model:

Square dimensions	7 × 7
Thickness	1.0
Centrifugal axis of rotation	(0, 1, 0) through origin
Coriolis axis of rotation	(0, 0, 1) through origin
Gravity load vector	(0, –1, 0)

Material:

Young's modulus	30 × 10⁶
Poisson's ratio	0.3
Coefficient of thermal expansion	0.0
Thermal conductivity	3.77 × 10^–5
Density	82.9
Sink (bulk fluid) temperature	75.0
Absolute zero temperature	–460.0

Initial conditions:

Initial velocity	ALL, 1, 10
	ALL, 2, 5
Hydrostatic pressure datum	3.0
Hydrostatic pressure elevation	0.0

Results and discussion

The calculated reactions are in agreement with the applied loads.

Input files

ABAQUS/Standard input files

CPE4HT element load tests:

ece4thdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ece4thdr.inp

ROTA.

ece4thdk.inp

HP, P, F, R, S.

CPE4T element load tests:

ece4tfdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ece4tfdr.inp

ROTA.

ece4tfdk.inp

HP, P, F, R, S.

CPE8HT element load tests:

ece8thdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ece8thdr.inp

ROTA.

ece8thdk.inp

HP, P, F, R, S.

CPE8RHT element load tests:

ece8tydd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ece8tydr.inp

ROTA.

ece8tydk.inp

HP, P, F, R, S.

CPE8RT element load tests:

ece8trdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ece8trdr.inp

ROTA.

ece8trdk.inp

HP, P, F, R, S.

CPE8T element load tests:

ece8tfdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ece8tfdr.inp

ROTA.

ece8tfdk.inp

HP, P, F, R, S.

CPEG3HT element load tests:

ecg3thdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, P1, HP1, R1, S1.

ecg3thdr.inp

ROTA.

ecg3thdk.inp

HP, P, F, R, S.

CPEG3T element load tests:

ecg3tfdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, P1, HP1, R1, S1.

ecg3tfdr.inp

ROTA.

ecg3tfdk.inp

HP, P, F, R, S.

CPEG4HT element load tests:

ecg4thdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ecg4thdr.inp

ROTA.

ecg4thdk.inp

HP, P, F, R, S.

CPEG4RHT element load tests:

ecg4tydd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ecg4tydr.inp

ROTA.

ecg4tydk.inp

HP, P, F, R, S.

CPEG4RT element load tests:

ecg4trdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ecg4trdr.inp

ROTA.

ecg4trdk.inp

HP, P, F, R, S.

CPEG4T element load tests:

ecg4tfdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ecg4tfdr.inp

ROTA.

ecg4tfdk.inp

HP, P, F, R, S.

CPEG6MHT element load tests:

ecg6tldd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, F1, F2, F3, P1, P2, P3, HP1, HP2, HP3,R1, R2, R3, S1, S2, S3.

ecg6tldd_po.inp

*POST OUTPUT analysis.

ecg6tldr.inp

ROTA.

ecg6tldk.inp

HP, P, F, R, S.

CPEG6MT element load tests:

ecg6tkdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, F1, F2, F3, P1, P2, P3, HP1, HP2, HP3,R1, R2, R3, S1, S2, S3.

ecg6tkdr.inp

ROTA.

ecg6tkdk.inp

HP, P, F, R, S.

CPEG8HT element load tests:

ecg8thdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ecg8thdr.inp

ROTA.

ecg8thdk.inp

HP, P, F, R, S.

CPEG8RHT element load tests:

ecg8tydd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ecg8tydr.inp

ROTA.

ecg8tydk.inp

HP, P, F, R, S.

CPEG8T element load tests:

ecg8tfdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ecg8tfdr.inp

ROTA.

ecg8tfdk.inp

HP, P, F, R, S.

CPS4T element load tests:

ecs4tfdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ecs4tfdr.inp

ROTA.

ecs4tfdk.inp

HP, P, F, R, S.

CPS8RT element load tests:

ecs8trdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ecs8trdr.inp

ROTA.

ecs8trdk.inp

HP, P, F, R, S.

CPS8T element load tests:

ecs8tfdd.inp

BX, BY, BF, GRAV, CENT, CENTRIF, CORIO, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

ecs8tfdr.inp

ROTA.

ecs8tfdk.inp

HP, P, F, R, S.

ABAQUS/Explicit input files

CPE3T element load tests:

coupledtempload_xpl_cpe3t.inp

BX, BY, BF, GRAV, F1, F2, F3, P1, P2, P3, R1, R2, R3, S1, S2, S3.

coupledtempload_s_xpl_cpe3t.inp

Same as coupledtempload_xpl_cpe3t.inp except with surface-based loads.

CPE4RT element load tests:

coupledtempload_xpl_cpe4rt.inp

BX, BY, BF, GRAV, F1, F2, F3, F4, P1, P2, P3, P4, R1, R2, R3, R4, S1, S2, S3, S4.

coupledtempload_s_xpl_cpe4rt.inp

Same as coupledtempload_xpl_cpe4rt.inp except with surface-based loads.

CPE6MT element load tests:

coupledtempload_xpl_cpe6mt.inp

BX, BY, BF, GRAV, F1, F2, F3, P1, P2, P3, R1, R2, R3, S1, S2, S3.

coupledtempload_s_xpl_cpe6mt.inp

Same as coupledtempload_xpl_cpe6mt.inp except with surface-based loads.

CPS3T element load tests:

coupledtempload_xpl_cps3t.inp

BX, BY, BF, GRAV, F1, F2, F3, P1, P2, P3, R1, R2, R3, S1, S2, S3.

coupledtempload_s_xpl_cps3t.inp

Same as coupledtempload_xpl_cps3t.inp except with surface-based loads.

CPS4RT element load tests:

coupledtempload_xpl_cps4rt.inp

BX, BY, BF, GRAV, F1, F2, F3, F4, P1, P2, P3, P4, R1, R2, R3, R4, S1, S2, S3, S4.

coupledtempload_s_xpl_cps4rt.inp

Same as coupledtempload_xpl_cps4rt.inp except with surface-based loads.

CPS6MT element load tests:

coupledtempload_xpl_cps6mt.inp

BX, BY, BF, GRAV, F1, F2, F3, P1, P2, P3, R1, R2, R3, S1, S2, S3.

coupledtempload_s_xpl_cps6mt.inp

Same as coupledtempload_xpl_cps6mt.inp except with surface-based loads.

III. Coupled temperature-displacement axisymmetric solid elements

Problem description

Model:

Planar dimensions	7 × 7
Inside radius	1.0
Centrifugal axis of rotation	(0, 1, 0) through origin
Gravity load vector	(0, –1, 0)

Mesh:

Linear elements	2 elements in radial direction
Quadratic elements	1 element in radial direction

Material:

Young's modulus	30 × 10⁶
Poisson's ratio	0.3
Coefficient of thermal expansion	0.0
Thermal conductivity	3.77 × 10^–5
Density	82.9
Sink (bulk fluid) temperature	75.0
Absolute zero temperature	–460.0

Initial conditions:

Hydrostatic pressure datum	3.0
Hydrostatic pressure elevation	0.0

Results and discussion

The calculated reactions are in agreement with the applied loads.

Input files

ABAQUS/Standard input files

CAX4HT element load tests:

eca4thdd.inp

BR, BZ, BF, GRAV, CENT, CENTRIF, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca4thdk.inp

HP, P, F, R, S.

CAX4T element load tests:

eca4tfdd.inp

BR, BZ, BF, GRAV, CENT, CENTRIF, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca4tfdk.inp

HP, P, F, R, S.

CAX8HT element load tests:

eca8thdd.inp

BR, BZ, BF, GRAV, CENT, CENTRIF, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca8thdk.inp

HP, P, F, R, S.

CAX8RHT element load tests:

eca8tydd.inp

BR, BZ, BF, GRAV, CENT, CENTRIF, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca8tydk.inp

HP, P, F, R, S.

CAX8RT element load tests:

eca8trdd.inp

BR, BZ, BF, GRAV, CENT, CENTRIF, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca8trdk.inp

HP, P, F, R, S.

CAX8T element load tests:

eca8tfdd.inp

BR, BZ, BF, GRAV, CENT, CENTRIF, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca8tfdk.inp

HP, P, F, R, S.

ABAQUS/Explicit input files

CAX3T element load tests:

coupledtempload_xpl_cax3t.inp

BR, BZ, BF, GRAV, F1, F2, F3, P1, P2, P3, R1, R2, R3, S1, S2, S3.

coupledtempload_s_xpl_cax3t.inp

Same as coupledtempload_xpl_cax3t.inp except with surface-based loads.

CAX4RT element load tests:

coupledtempload_xpl_cax4rt.inp

BR, BZ, BF, GRAV, F1, F2, F3, F4, P1, P2, P3, P4, R1, R2, R3, R4, S1, S2, S3, S4.

coupledtempload_s_xpl_cax4rt.inp

Same as coupledtempload_xpl_cax4rt.inp except with surface-based loads.

CAX6MT element load tests:

coupledtempload_xpl_cax6mt.inp

BR, BZ, BF, GRAV, F1, F2, F3, P1, P2, P3, R1, R2, R3, S1, S2, S3.

coupledtempload_s_xpl_cax6mt.inp

Same as coupledtempload_xpl_cax6mt.inp except with surface-based loads.

IV. Coupled temperature-displacement three-dimensional elements

Problem description

Model:

Cubic dimensions	7 × 7 × 7
Centrifugal axis of rotation	(0, 1, 0) through (–1000, 3.5, –3.5)
Gravity load vector	(1, 2, 3)

Material:

Young's modulus	30 × 10⁶
Poisson's ratio	0.3
Coefficient of thermal expansion	0.0
Thermal conductivity	3.77 × 10^–5
Density	82.9
Sink (bulk fluid) temperature	75.0
Absolute zero temperature	–460.0

Initial conditions:

Hydrostatic pressure datum	0.0
Hydrostatic pressure elevation	–7.0

Results and discussion

The calculated reactions are in agreement with the applied loads.

Input files

ABAQUS/Standard input files

C3D8T element load tests:

ec38tfdd.inp

BX, BY, BZ, BF, GRAV, CENT, CENTRIF, F1, F2, F3, F4, F5, F6, P1, P2, P3, P4, P5, P6, HP1, HP2, HP3, HP4, HP5, HP6, R1, R2, R3, R4, R5, R6,S1, S2, S3, S4, S5, S6.

ec38tfdr.inp

ROTA.

ec38tfdk.inp

HP, P, F, R, S.

C3D8HT element load tests:

ec38thdd.inp

BX, BY, BZ, BF, GRAV, CENT, CENTRIF, F1, F2, F3, F4, F5, F6, P1, P2, P3, P4, P5, P6, HP1, HP2, HP3, HP4, HP5, HP6, R1, R2, R3, R4, R5, R6,S1, S2, S3, S4, S5, S6.

ec38thdd_po.inp

*POST OUTPUT analysis.

ec38thdr.inp

ROTA.

ec38thdk.inp

HP, P, F, R, S.

C3D20T element load tests:

ec3ktfdd.inp

BX, BY, BZ, BF, GRAV, CENT, CENTRIF, F1, F2, F3, F4, F5, F6, P1, P2, P3, P4, P5, P6, HP1, HP2, HP3, HP4, HP5, HP6, R1, R2, R3, R4, R5, R6,S1, S2, S3, S4, S5, S6.

ec3ktfdr.inp

ROTA.

ec3ktfdk.inp

HP, P, F, R, S.

C3D20HT element load tests:

ec3kthdd.inp

BX, BY, BZ, BF, GRAV, CENT, CENTRIF, F1, F2, F3, F4, F5, F6, P1, P2, P3, P4, P5, P6, HP1, HP2, HP3, HP4, HP5, HP6, R1, R2, R3, R4, R5, R6,S1, S2, S3, S4, S5, S6.

ec3kthdr.inp

ROTA.

ec3kthdk.inp

HP, P, F, R, S.

C3D20RT element load tests:

ec3ktrdd.inp

BX, BY, BZ, BF, GRAV, CENT, CENTRIF, F1, F2, F3, F4, F5, F6, P1, P2, P3, P4, P5, P6, HP1, HP2, HP3, HP4, HP5, HP6, R1, R2, R3, R4, R5, R6,S1, S2, S3, S4, S5, S6.

ec3ktrdr.inp

ROTA.

ec3ktrdk.inp

HP, P, F, R, S.

C3D20RHT element load tests:

ec3ktydd.inp

BX, BY, BZ, BF, GRAV, CENT, CENTRIF, F1, F2, F3, F4, F5, F6, P1, P2, P3, P4, P5, P6, HP1, HP2, HP3, HP4, HP5, HP6, R1, R2, R3, R4, R5, R6,S1, S2, S3, S4, S5, S6.

ec3ktydr.inp

ROTA.

ec3ktydk.inp

HP, P, F, R, S.

ABAQUS/Explicit input files

C3D4T element load tests:

coupledtempload_xpl_c3d4t.inp

BX, BY, BZ, BF, GRAV, F1, F2, F3, F4, P1, P2, P3, P4, R1, R2, R3, R4, S1, S2, S3, S4.

coupledtempload_s_xpl_c3d4t.inp

Same as coupledtempload_xpl_c3d4t.inp except with surface-based loads.

C3D6T element load tests:

coupledtempload_xpl_c3d6t.inp

BX, BY, BZ, BF, GRAV, F1, F2, F3, F4, F5, P1, P2, P3, P4, P5, R1, R2, R3, R4, R5, S1, S2, S3, S4, S5.

coupledtempload_s_xpl_c3d6t.inp

Same as coupledtempload_xpl_c3d6t.inp except with surface-based loads.

C3D8RT element load tests:

coupledtempload_xpl_c3d8rt.inp

BX, BY, BZ, BF, GRAV, F1, F2, F3, F4, F5, F6, P1, P2, P3, P4, P5, P6, R1, R2, R3, R4, R5, R6, S1, S2, S3, S4, S5, S6.

coupledtempload_s_xpl_c3d8rt.inp

Same as coupledtempload_xpl_c3d8rt.inp except with surface-based loads.

V. Coupled temperature-displacement axisymmetric shell element

Problem description

Model:

Length	10.0
Radius	5.0
Thickness	0.5
Centrifugal axis of rotation	(0, 1, 0) through origin
Gravity load vector	(0, 1, 0)

Material:

Young's modulus	3 × 10⁶
Poisson's ratio	0.3
Thermal conductivity	3.77 × 10^–5
Density	82.9
Sink (bulk fluid) temperature	75.0
Absolute zero temperature	–460.0

Initial conditions:

Hydrostatic pressure datum	7.0
Hydrostatic pressure elevation	0.0

Results and discussion

The calculated reactions are in agreement with the applied loads.

Input files

esa3txdd.inp

SAX2T: BR, BZ, BF, GRAV, CENT, CENTRIF, FNEG, FPOS, P, HP, RNEG, RPOS, SNEG, SPOS.

esa3txdk.inp

SAX2T: HP, P, F, R, S.

VI. Coupled temperature-displacement general shell element

Problem description

Model:

Planar dimensions	7 × 7
Thickness	2.0
Centrifugal and Coriolis axes of rotation	(0, 1, 0) through origin
Gravity load vector	(0, 1, 0)

Material:

Young's modulus	3 × 10⁶
Poisson's ratio	0.3
Thermal conductivity	3.77 × 10^–5
Density	82.9
Sink (bulk fluid) temperature	75.0
Absolute zero temperature	–460.0

Initial conditions:

Hydrostatic pressure datum	7.0
Hydrostatic pressure elevation	0.0

Results and discussion

The calculated reactions are in agreement with the applied loads.

Input files

es38txdd.inp

S8RT: BX, BY, BZ, BF, GRAV, CENT, CENTRIF, FNEG, FPOS, P, HP, RNEG, RPOS, SNEG, SPOS.

es38txdr.inp

S8RT: ROTA.

es38txdk.inp

S8RT: HP, P, F, R, S.

VII. Coupled temperature-displacement axisymmetric twist elements

Problem description

Model:

Planar dimensions	7 × 7
Inside radius	1.0
Centrifugal axis of rotation	(0, 1, 0) through origin
Gravity load vector	(0, –1, 0)

Mesh:

Linear elements	2 elements in radial direction
Quadratic elements	1 element in radial direction

Material:

Young's modulus	30 × 10⁶
Poisson's ratio	0.3
Coefficient of thermal expansion	0.0
Thermal conductivity	3.77 × 10^–5
Density	82.9
Sink (bulk fluid) temperature	75.0
Absolute zero temperature	–460.0

Initial conditions:

Hydrostatic pressure datum	3.0
Hydrostatic pressure elevation	0.0

Results and discussion

The calculated reactions are in agreement with the applied loads.

Input files

CGAX3T element load tests:

eca3hfdd.inp

BR, BZ, BF, CENT, CENTRIF, GRAV, F1, F2, F3, P1, P2, P3, HP1, HP2, HP3, R1, R2, R3, S1, S2, S3.

eca3hfdk.inp

HP, P, F, R, S.

CGAX3HT element load tests:

eca3hhdd.inp

BR, BZ, BF, CENT, CENTRIF, GRAV, F1, F2, F3, P1, P2, P3, HP1, HP2, HP3, R1, R2, R3, S1, S2, S3.

eca3hhdk.inp

HP, P, F, R, S.

CGAX4T element load tests:

eca4hfdd.inp

BR, BZ, BF, CENT, CENTRIF, GRAV, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca4hfdk.inp

HP, P, F, R, S.

CGAX4HT element load tests:

eca4hhdd.inp

BR, BZ, BF, CENT, CENTRIF, GRAV, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca4hhdk.inp

HP, P, F, R, S.

CGAX4RT element load tests:

eca4hrdd.inp

BR, BZ, BF, CENT, CENTRIF, GRAV, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca4hrdk.inp

HP, P, F, R, S.

CGAX4RHT element load tests:

eca4hydd.inp

BR, BZ, BF, CENT, CENTRIF, GRAV, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca4hydk.inp

HP, P, F, R, S.

CGAX6MT element load tests:

eca6hfdd.inp

BR, BZ, BF, CENT, CENTRIF, GRAV, F1, F2, P1, P2, HP1, HP2, R1, R2, S1, S2.

eca6hfdk.inp

HP, P, F, R, S.

CGAX6MHT element load tests:

eca6hhdd.inp

BR, BZ, BF, CENT, CENTRIF, GRAV, F1, F2, P1, P2, HP1, HP2, R1, R2, S1, S2.

eca6hhdk.inp

HP, P, F, R, S.

CGAX8T element load tests:

eca8hfdd.inp

BR, BZ, BF, CENT, CENTRIF, GRAV, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca8hfdk.inp

HP, P, F, R, S.

CGAX8HT element load tests:

eca8hhdd.inp

BR, BZ, BF, CENT, CENTRIF, GRAV, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca8hhdk.inp

HP, P, F, R, S.

CGAX8RT element load tests:

eca8hrdd.inp

BR, BZ, BF, CENT, CENTRIF, GRAV, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca8hrdk.inp

HP, P, F, R, S.

CGAX8RHT element load tests:

eca8hydd.inp

BR, BZ, BF, CENT, CENTRIF, GRAV, F1, F2, F3, F4, P1, P2, P3, P4, HP1, HP2, HP3, HP4, R1, R2, R3, R4, S1, S2, S3, S4.

eca8hydk.inp

HP, P, F, R, S.