Use the Engine Mesh tool to define the engine or missile modeling and
meshing.
From the Aeroelasticity ribbon, click the
Engine Mesh tool.
Figure 1.
Select Point 1 (x, y, z), the origin of the panel (cylinder).
Select Point 2 (x, y, z) to define the length of the engine body in the local x
direction (x12).
In the microdialog , define the number of span elements
for each interference panel (NSPAN).
In the microdialog , define the number of chord elements
for each interference panel (NCHORD).
In the microdialog , define the number of interference
elements (NINT).
In the microdialog , enter the constant half width of
the body.
Select the aerospace coordinate system CP to define the axis of the body.
The CAERO1 ID (EID) represents the element start ID with ID spanning along the
body circumference.
Figure 2.
Set options as necessary by clicking on the guide bar .
On the guide bar , click one of the following:
- Save changes and stay in the tool
- Save changes and close the tool
Tip:
From the Aeroelasticity ribbon, click the satellite
icon that appears
when you hover over the Engine Mesh tool to open the Aeroelasticity Browser .