Use the Body Mesh tool to define the body type of aerospace meshing called
CAERO2.
Restriction: Only applicable for the Nastran (MSC) solver.
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From the Aeroelasticity ribbon, click the
Body Mesh tool.
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Select point 1 (x, y, z), the origin of the panel (cylinder).
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Select point 2 (x, y, z) to define the length of the body in the local x
direction (x12).
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In the microdialog, define the number of slender body
elements (NSB).
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In the microdialog, define the number of interference
elements (NINT).
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In the microdialog, define the length of the slender
body division (LSB), if NSB is zero/undefined.
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In the microdialog, define the length of interference
(LINT), if NINT is zero/undefined.
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Select the aerospace coordinate system CP to define the axis of the body.
The CAERO2 ID (EID) represents the element start ID with ID spanning along the
body circumference.
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Set options as necessary by clicking
on the guide bar.
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On the guide bar, click one of the following:
- Save changes/create mesh
and stay in the tool
- Save changes/create mesh
and close the tool
Tip:
- From the Aeroelasticity ribbon, click the satellite
icon
that appears when you hover over the Body Mesh tool
to open the Aeroelasticity Browser.