Can Void Volume Ratio Override computed data be displayed for each subslice?
This is based on the radial distance from the center of the fiber or particle
within the interphase.
Increases the capacity of this vector, if necessary, to ensure that
it can hold at least the number of components specified
by the minimum capacity argument.
Either MaterialProperty.PROPERTY_TYPE_FIBER or
MaterialProperty.PROPERTY_TYPE_PARTICLE: used to
determine whether the analysis is 2D or 3D, respectively.
Either MaterialProperty.PROPERTY_TYPE_FIBER or
MaterialProperty.PROPERTY_TYPE_PARTICLE: used to
determine whether the analysis is 2D or 3D, respectively.
Either MaterialProperty.PROPERTY_TYPE_FIBER or
MaterialProperty.PROPERTY_TYPE_PARTICLE: used to
determine whether the analysis is 2D or 3D, respectively.
Either MaterialProperty.PROPERTY_TYPE_FIBER or
MaterialProperty.PROPERTY_TYPE_PARTICLE: used to
determine whether the analysis is 2D or 3D, respectively.
Either MaterialProperty.PROPERTY_TYPE_FIBER or
MaterialProperty.PROPERTY_TYPE_PARTICLE: used to
determine whether the analysis is 2D or 3D, respectively.
Either MaterialProperty.PROPERTY_TYPE_FIBER or
MaterialProperty.PROPERTY_TYPE_PARTICLE: used to
determine whether the analysis is 2D or 3D, respectively.
Get the factor number (subscript) of the MFIM item
corresponding to the given four-character code
used to identify the Multi-Factor Interaction Model (MFIM) factor.
Get the subscript in the void volume ratio override Vector
given the ply and whether it is the primary or secondary material
for which an override may be defined.
Constructor creates window to display text area containing messages
but just after a line containing a series of dollar signs
and the given character string.
Array of column widths for TextFields in the GridBag Layout
showing that TextFields containing material ID's are smaller than
TextFields containing numeric values for the volume ratios.
Enter/Modify Data for ICAN/JAVA:
Displays a sequence of screens prompting the user
for the data necessary to run the Integrated Composite
Analyzer (ICAN/JAVA) program.
Detects when the following keys are released from the keyboard:
Shift+Tab, Tab, Enter, Up Arrow, Down Arrow
F1, Alt+Right, Alt+Left, Ctrl-End, and Ctrl-Home
Mechanical static applied load: bending load xx, in lb-inch/inch or kg-meter/meter;
or mechanical displacement curvature, in inches/inch or meters/meter.
Mechanical static applied load: bending load xy, in lb-inch/inch or kg-meter/meter;
or mechanical displacement curvature, in inches/inch or meters/meter.
Mechanical static applied load: bending load yy, in lb-inch/inch or kg-meter/meter;
or mechanical displacement curvature, in inches/inch or meters/meter.
This composite material system ID is a code associated with
some composite material fabricated from Fibers and Matrix
or Particles and Binder under the specified conditions.
Material ID may be either a non-Fiber, non-Particle, entry
in the Material DataBank or a composite material ID which
matches the value on the composite Material System input form.
Display wait screen, reset input and output data,
read new input data, validate input data, remove wait screen,
and proceed to enter/modify ICAN/JAVA data screen.
Value used to indicate that the list of colors for drawing
will have hues cycling through the colors from red to magenta
keeping the spacing between adjacent hues widely spearated.
Set the desired focus to some component,
set the color for nearby blank material ID,
make the component visible by scrolling to it,
and request the focus to the desired component.
Get a line of the table containing:
thickness,
position,
fiber volume ratio,
interphase volume ratio,
matrix volume ratio,
fiber area,
interphase area,
matrix area.
Get a line of the subslice table containing:
thicknesses,
positions,
fiber volume ratio,
interphase volume ratio,
matrix volume ratio,
fiber area,
interphase area,
matrix area.
Micromechanics equations for high temperature Fiber-reinforced
metal matrix composites, from NASA Technical Memorandum 102107,
with Fiber, Matrix, and Interphase.
Micromechanics equations for high temperature Fiber-reinforced
metal matrix composites, from NASA Technical Memorandum 102107,
with Fiber, Matrix, and Interphase.
Micromechanics equations for high temperature Fiber-reinforced
metal matrix composites, from NASA Technical Memorandum 104346,
with Fiber, Matrix, and Interphase.
2D Micromechanics equations for high temperature Fiber-reinforced
metal matrix composites, from NASA Technical Memorandum 104346,
with Fiber, Matrix, and Interphase.
Micromechanics equations for high temperature Fiber-reinforced
metal matrix composites, from NASA Technical Memorandum 87154,
with Fiber, Matrix, and Interphase.
Computes micromechanics equations for Fiber-reinforced ceramic
matrix composites, from NASA Technical Paper 3602, with
Fiber, but without Matrix or Interphase.
Computes micromechanics equations for Fiber-reinforced ceramic
matrix composites, from NASA Technical Paper 3602, with
Matrix and Fiber, but without Interphase.
Computes micromechanics equations for Fiber-reinforced ceramic
matrix composites, from NASA Technical Paper 3602, with
Matrix and Interphase, but without Fiber.
Computes micromechanics equations for Fiber-reinforced ceramic
matrix composites, from NASA Technical Paper 3602, with
Matrix and Fiber, but without Interphase.
Computes micromechanics equations for Fiber-reinforced ceramic
matrix composites, from NASA Technical Paper 3602, with
Matrix and Interphase, but without Fiber.