4.4.5. Directed Energy

Aria contains a number of directed energy (laser) source and flux models. The BEGIN DIRECTED ENERGY block in the Aria Region provides a unified way of specifying these sources and fluxes for a given configuration.

A directed energy model can be implemented as a surface flux, a source that penetrates into the surface, or a combination of the two. The typical inputs for a directed energy model are:

  • LASER POWER - The total power of the laser in Watts (for problems in SI MKS units). If there are multiple sources/fluxes specified the total power is divided among them based on their individual efficiency values (which must sum to 1).

  • PATH FUNCTION - A piecewise linear function for the time-varying position and orientation of the laser source.

  • ORIGIN AND NORMAL FUNCTION - A piecewise linear function for the time-varying position and orientation of the laser flux.

  • BEGIN X SOURCE - A sub-block defining a source model to use and its relevant parameters.

  • BEGIN X POWER WELD FLUX - A sub-block defining a flux model to use and its relevant parameters.

The complete set of commands for the directed energy model can be found in the directed energy command reference. An example input block is shown below for a case using both a source term and flux term in the same block.

BEGIN DIRECTED ENERGY MODEL bc2
  laser_power = CONSTANT Value = 1500

  add volume block_1    # for the source
  path function = path1 # for the source

  add surface surface_1 # for the flux
  Origin and Normal function = path2 # for the flux

  BEGIN Sharp Power Weld Flux
    efficiency = 0.5
    beam diameter = 0.20
  END

  BEGIN hemisphere source
    efficiency = 0.5
    beam diameter = 0.20
  END
END

4.4.5.1. Laser Path

The movement of the laser source and flux are controlled by multicolumn user-defined functions, in the format shown below.

Begin Definition for Function my_path
  Type is multicolumn piecewise linear
  Column Titles Time X Y Z nx ny nz
  Begin Values
    0.0   2.2e-2  5e-3  1.5e-2 0 1 0
    4.0   2.2e-2  1e-3 -1.5e-2 0 1 0
    8.0   2.2e-2  1e-3 -1.5e-2 0 1 0
  End
End

The laser sources/fluxes will follow the path defined by this function and the first and last rows of the table define the start and end times and positions. Outside those times, the laser is off and there is no source or flux.

Note

Both the PATH FUNCTION and ORIGIN AND NORMAL FUNCTION expect functions of this format. The PATH FUNCTION is used for sources while ORIGIN AND NORMAL FUNCTION is used for boundary fluxes.

Note

For laser fluxes the path normal vector should be the direction of the laser, and its orientation (towards or away from the surface) does not matter. The laser path origin should be the point where the laser originates from (so the laser vector is defined by the point and normal).

Note

For laser sources, the normal is optional and is used to define the source depth direction, and it should be pointed away from the surface (so the source depth is in the opposite direction as the normal). The laser path point is the center of the source (e.g. the center of the sphere for a spherical source).

4.4.5.2. Source Models

The various types of laser sources available are described in the following sections. For a complete list of the commands required for each model, refer to the directed energy command summary.

4.4.5.2.1. Hemispherical

The hemisphere model defines a hemispherical volume to heat the material block. If a Gaussian distribution is selected, the model is defined as:

q_{hemisphere} = \frac{6\sqrt{3}\eta P }{r_{beam}^{3}\pi\sqrt{\pi}}\exp{\left(-3\left(\frac{r^{2}}{r_{beam}^{2}}\right)\right)}

where r_{beam} is the beam radius, r is the minimum distance from the evaluation point to the laser focal spot, \eta is the efficiency and P is the laser power. If the uniform distribution is selected, then the model is defined as:

q_{hemisphere} = \frac{3\eta P}{2\pi r_{beam}^{3}}

The figure below shows a schematic of the hemispherical heating source.

Hemispherical source geometry

Fig. 4.19 Hemispherical source geometry.

4.4.5.2.2. Spherical

The sphere model defines a spherical volume to heat the material block. If a Gaussian distribution is selected, the model is defined as:

q_{sphere} = \frac{3\sqrt{3}\eta P }{r_{beam}^{3}\pi\sqrt{\pi}}\exp{\left(-3\left(\frac{r^{2}}{r_{beam}^{2}}\right)\right)}

where r_{beam} is the beam radius, r is the minimum distance from the evaluation point to the laser focal spot, \eta is the efficiency and P is the laser power. If the uniform distribution is selected, then the model is defined as:

q_{sphere} = \frac{3\eta P}{4\pi r_{beam}^{3}}

The figure below shows a schematic of the spherical heating source.

Spherical source geometry

Fig. 4.20 Spherical source geometry.

4.4.5.2.3. Beer-Lambert

The Beer-Lambert model assumes an exponential decrease of the laser absorptivity with penetration depth. It is defined as:

q_{BL} = \frac{\eta r_{eff} P}{\pi r_{beam}^{2} \beta^{2} (1 - \exp{(-r_{eff})})} \exp{\left(-r_{eff}\left(\frac{r_{p}^{2}}{r_{beam}^{2}}\right)\right)} I_{att}

where r_{eff} the effective beam radius, r_{beam} is the beam radius P is the laser power, \beta is a spatial factor, r_{p} is the planar distance from the evaluation point to the laser focal point and I_{att} is an attenuation factor that varies exponentially with depth. The spatial factor \beta is an optional parameter defined by SPATIAL INFLUENCE FACTOR, and is given a default value of 1. The attenuation factor I_{att} is defined as:

I_{att} = \frac{\alpha \exp{\left( -(z - z_{c})\alpha \right)}}{1-\exp{(-\alpha z_{max})}}

where \alpha is an absorption coefficient (1/L) of range roughly 1 to 1e6 defined as a material property for the volume of interest. The value z_{c} is the z position of the laser focal point and z_{max} is the maximum penetration depth, which is currently defined as z_{max} = 6r_{beam}. Surface absorption of energy can be accounted for by defining a modified attenuation factor \eta I_{att} where \eta is the efficiency parameter.

4.4.5.2.4. Parallelpiped

The parallelpiped model is defined as:

q_{parallelpiped} = \frac{\eta P}{4abc}

where a is the travel semi axis, b is the width semi axis, c is the penetration depth, \eta is the efficiency and P is the laser power. The parallelpiped assumes a uniform distribution. The figure below shows a schematic of the parallelpiped heating source.

Parallelpiped source geometry

Fig. 4.21 Parallelpiped source geometry.

4.4.5.2.5. Ellipsoid

The ellipsoid model is defined as:

q_{ellipsoid} = \frac{6\sqrt{3}\eta P }{abc\pi\sqrt{\pi}}\exp{\left(-3\left(\frac{(x-x_{c})^{2}}{a^{2}} + \frac{(y-y_{c})^{2}}{b^{2}} + \frac{(z-z_{c})^{2}}{c^{2}}\right)\right)}

where a is the travel semi-axis, b is the width semi-axis, c is the depth semi-axis, \eta is the efficiency, P is the laser power and x_{c}, y_{c}, and z_{c} are the x, y, and z coordinate of the laser focal point, respectively. The figure below shows a schematic of the ellipsoid heating source, where the width semi-axis is pointing out of the page.

Ellipsoid source geometry

Fig. 4.22 Ellipsoid source geometry.

4.4.5.2.6. Double Ellipsoid

The double ellipsoid model defines two ellipsoid energy sources, q_{ellipsoid,fore} and q_{ellipsoid,aft} combined at the laser focal point. The fore ellipsoidal energy source is defined as:

q_{ellipsoid,fore} = \frac{6\sqrt{3}\eta P f_{fore}}{a_{fore}bc\pi\sqrt{\pi}}\exp{\left(-3\left(\frac{(x-x_c)^{2}}{a_{fore}^{2}} + \frac{(y - y_c)^{2}}{b^{2}} + \frac{(z - z_c)^{2}}{c^{2}}\right)\right)}

where a_{fore} is the fore travel semi-axis, b is the width semi-axis, c is the depth semi-axis, f_{fore} is the fore power fraction, \eta is the efficiency P is the laser power, and x_{c}, y_{c} and z_{c} are the x, y and z coordinate of the laser focal point, respectively. The aft ellipsoidal energy source is defined as:

q_{ellipsoid,aft} = \frac{6\sqrt{3}\eta P f_{aft}}{a_{aft}bc\pi\sqrt{\pi}}\exp{\left(-3\left(\frac{(x - x_c)^{2}}{a_{aft}^{2}} + \frac{(y-y_c)^{2}}{b^{2}} + \frac{(z-z_c)^{2}}{c^{2}}\right)\right)}

where a_{aft} is the fore travel semi-axis and f_{aft} is the aft power fraction. The figure below shows a schematic of the double ellipsoid energy source model, where the width semi-axis is pointing out of the page.

Double ellipsoid source geometry

Fig. 4.23 Double ellipsoid source geometry.

4.4.5.2.7. Conical

The conical heat source model is defined as:

q_{conical} = \frac{9\exp{(3)}\eta}{\pi d(\exp{(3)} - 1)(r_{s}^{2} + r_{s}r_{d} + r_{d}^{2})} \exp{\left(\frac{-r_{p}^{2}}{r_{0}^{2}}\right)}

where \eta is the efficiency, d is the penetration depth, r_{s} is the beam radius at the laser focal point, r_{d} is the beam radius at penetration depth d and r_{p} is the planar distance from the evaluation point to the laser focal point. The term r_{0} is the beam radius at a particular depth z, and is defined as:

r_{0} = r_{s} - (r_{s} - r_{d})\left(\frac{z-z_{c}}{d}\right)

where z_{c} is the z position of the laser focal point. The figure below shows a schematic of the conical energy source model.

Conical source geometry

Fig. 4.24 Conical source geometry.

4.4.5.3. Flux Models

The various types of laser flux models available are described in the following sections. For a complete list of the commands required for each model, refer to the directed energy command summary.

4.4.5.3.1. Sharp

The coordinates of the center of the beam are provided by the X, Y, and Z components of the provided origin_and_normal_function. The direction of the beam is provided by the NX, NY, and NZ components of the origin_and_normal_function. The applied flux is given by:

\frac{(-\n)\bcdot\vector{d}}{|\vector{d}|}\frac{\alpha e P}{\pi R^2}

P is the laser power defined for the material, R is the beam radius, \alpha is the laser absorptivity defined for the material, e is the EFFICIENCY, and the term -\n\bcdot\vector{d} accounts for the fact that the surface may not be orthogonal to the laser. Points with values of r_p > CLIP_RADIUS will receive zero flux. r_p is the shortest distance between a point on the surface and the line defined by the beam origin and normal. If ACTIVATION is set to true, points whose temperature exceed ACTIVATION_TEMPERATURE will be flagged as activated for use with the ACTIVATION USER FUNCTION thermal conductivity model. If INTEGRATED is true, this flux will be integrated between the previous time step and the current one and the average flux applied.

4.4.5.3.2. Gaussian

The coordinates of the center of the beam are provided by the X, Y, and Z components of the provided origin_and_normal_function. The direction of the beam is provided by the NX, NY, and NZ components of the origin_and_normal_function. The applied flux is given by:

\frac{(-\n)\bcdot\vector{d}}{|\vector{d}|}\frac{\alpha e R_{eff} P}{\pi R^2 (1 - e^{-R_{eff}})}e^{-R_{eff}\frac{r_p^2}{R^2}}

P is the laser power defined for the material, R is the beam radius, R_{eff} is the effective beam radius, \alpha is the laser absorptivity defined for the material, e is the EFFICIENCY, and r_p is the shortest distance between a point on the surface and the line defined by the beam origin and normal. The term -\n\bcdot\vector{d} accounts for the fact that the surface may not be orthogonal to the laser. Points with values of r_p > CLIP_RADIUS will receive zero flux. If ACTIVATION is set to true, points whose temperature exceed ACTIVATION_TEMPERATURE will be flagged as activated for use with the ACTIVATION USER FUNCTION thermal conductivity model. If INTEGRATED is true, this flux will be integrated between the previous time step and the current one and the average flux applied.