Constitutive law for unilateral thermo-mechanical contact
Thermo-mechanical analysis of problems involving unilateral contact between two bodies. Coulomb dry friction law is used. The contact condition is enforced via a penalty method or augmented Lagrangian method according to ISTRA(4). Heat transfer between the bodies depends upon the contact state.
Prepro: LCNTTH.F
Lagamine: COU2DC.F, COU3DC.F
Plane stress state | YES |
Plane strain state | YES |
Axisymmetric state | YES |
3D state | YES |
Generalized plane state | YES |
Line 1 (2I5, 60A1) | |
---|---|
IL | Law number |
ITYPE | 280 |
COMMENT | Any comment (up to 60 characters) that will be reproduced on the output listing. |
Line 1 (3I5) | |
---|---|
INDIC | 0, 1, 2 to define the outside temperature used in case of no contact (see Use paragraph) |
NINTV | 1 (except in 3D dynamic where value $\neq$ 1 is possible) For the 3D state dynamic analysis: Number of sub-steps used to integrate numerically the constitutive equation in a time step |
ISOL | 0, 1 or 4 |
NTEMP | Number of temperatures at which THCON, CONVEC & RADIA parameters are given (see hereafter). Default value = 1 |
if NTEMP = 1
Line 1 (7G10.0) | |
---|---|
AKP | penalty coefficient on the contact pressure $K_p$ |
AKTAU | penalty coefficient on the shear frictional stress $K_{\tau}$ |
PHI | COULOMB's friction coefficient $tg \phi $ |
B | cohesion |
TAUMAX | maximum contact friction (only for 2D state) (default value = $10^{20}$) |
THCON | thermal resistance when contact occurs |
CONVEC | convection coefficient h |
Line 2 (4G10.0) | |
RADIA | radiation coeficient $\sigma_0$ $\varepsilon$ where $\sigma_0$ is the Boltzman constant, and the $\varepsilon$ emissivity |
CTQ | TAYLOR QUINNEY's coefficient to take into account the dissipation for heat computation a. CTQ = -1 $\Rightarrow$ flux = QB(3) b. CTQ $\in$ [0,1] $\Rightarrow$ QB(3) = $\Sigma (DISSIP/2*CTQ*\Delta t)$ c. CTQ $\geq$ 100 $\Rightarrow$ flux = DISSIP/2*(CTQ-100) Case a = semi-coupled analysis : thermal analysis Case b = semi-coupled analysis : mechanical analysis Case c = total coupled analysis |
TAMB | atmosphere temperature |
PRESID | residual pressure |
if NTEMP > 1
Line 1 (5G10.0) | |
---|---|
AKP | penalty coefficient on the contact pressure $K_p$ |
AKTAU | penalty coefficient on the shear frictional stress $K_{\tau}$ |
PHI | COULOMB's friction coefficient $\phi$ |
B | cohesion |
TAUMAX | maximum contact friction (only for 2D state) (default value= $10^{20}$) |
Line 2 (4G10.0) - Repeated NTEMP times | |
TEMP | Temperature |
THCON | Thermal resistance when contact occurs |
CONVEC | convection coefficient h |
RADIA | radiation coeficient $\sigma_0$ $\varepsilon$ where $\sigma_0$ is the Boltzman constant, and the $\varepsilon$ emissivity |
Line NTEMP+2 (3G10.0) | |
CTQ | TAYLOR QUINNEY's coefficient to take into account the dissipation for heat computation a. CTQ = -1 $\Rightarrow$ flux = QB(3) b. CTQ $\in$ [0,1] $\Rightarrow$ QB(3) = $\Sigma (DISSIP/2*CTQ*\Delta t)$ c. CTQ $\geq$ 100 $\Rightarrow$ flux = DISSIP/2*(CTQ-100) Case a = semi-coupled analysis : thermal analysis Case b = semi-coupled analysis : mechanical analysis Case c = total coupled analysis |
TAMB | atmosphere temperature |
PRESID | residual pressure |
4 for 3D state
3 for the other cases
For the 3D state
SIG(1) | normal contact pressure |
SIG(2) | tangent contact stress in the $\xi$ direction |
SIG(3) | tangent contact stress in the $\eta$ direction |
SIG(4) | heat transfer |
The $\xi$ and $\eta$ correspond to the intrinsic co-ordinates of the contact element CFI3D
For the other cases
SIG(1) | normal contact pressure |
SIG(2) | tangent contact stress |
SIG(3) | heat transfer |
3
Q(1) | 0 if the current state is elastic (no sliding) 1 if the current state is elastoplastic (sliding at contact) -1 no mechanical, nor thermical contact |
Q(2) | amount of mechanical energy dissipated per unit area, due to friction |
Q(3) | information concerning the mechanical dissipation into heat flow (for exact meaning see CTQ parameter above) |