Amiga500
Aerospace
- Mar 6, 2009
- 3
Hi everyone,
I've a problem properly orientating a composite material in a cylinderical coordinate system, to explain:
The composites material orientation system is:
1 - longitudinal
2 - transverse
3 - through thickness.
For a Cartesian coord system, this corresponds to:
1 - x-axis
2 - y-axis
3 - z-axis
Which is OK.
But a cylindrical coordinate system, the internal mapping is:
1 - Radius-axis
2 - Theta-axis
3 - Z-axis
Which would mean for a composite the longitudinal material properties are mapped to the through-thickness axis, the transverse material properties mapped to the longitudinal axis and the through thickness material properties mapped to the transverse axis.
How do I change this mapping around to correctly reflect the material properties.
Thank you for your time.
Brendan
I've a problem properly orientating a composite material in a cylinderical coordinate system, to explain:
The composites material orientation system is:
1 - longitudinal
2 - transverse
3 - through thickness.
For a Cartesian coord system, this corresponds to:
1 - x-axis
2 - y-axis
3 - z-axis
Which is OK.
But a cylindrical coordinate system, the internal mapping is:
1 - Radius-axis
2 - Theta-axis
3 - Z-axis
Which would mean for a composite the longitudinal material properties are mapped to the through-thickness axis, the transverse material properties mapped to the longitudinal axis and the through thickness material properties mapped to the transverse axis.
How do I change this mapping around to correctly reflect the material properties.
Thank you for your time.
Brendan