When you create a study, the program automatically determines the mesh
			type to be solid, shell, or mixed based on the existing geometry. 
		Creating Shell Mesh 
			
			
						
							| Sheet Metals | Sheet metals with uniform
								thicknesses (except for drop test studies) are treated as shells
								automatically by the program. The software extracts the mid-surfaces
								and generates shell mesh at the mid-surface.  You also have the option to first treat sheet metals as solid
									bodies, and then convert manually selected solid faces to
									shells. | 
						
							| Surface Geometries | Surface geometries are treated as
								shells automatically by the program. You can control the position of
								the shell mesh to the top, middle, or bottom faces of the shell. To
								position the mesh to a reference surface, you can type an offset
								value. By default, the mesh is always aligned to
									the middle face of the shell.   See also
											Offsets for
									Shells. | 
						
							| Solid Parts | Solid parts are not meshed with
								shell elements. However, you can still create a surface geometry
								from a solid face. Do one of these: 
									Right-click a solid body, and select Define Shell
											by Selected Faces. In the Shell
											Definition PropertyManager, select a solid
										face to create a  shell surface. Define the thickness of the
										shell and the offset value to position the shell mesh.Open a part document and click . You then select the solid face to offset and
										specify the direction and offset distance.Click  to insert a midsurface between a pair of
										faces.  The program creates a mixed mesh
									automatically when different geometries are present in the
									model.  | 
					
Assigning Thickness
			
			
						
							| Sheet Metal | The program automatically extracts
								and assigns the thickness of the sheet metal to the shell. You
								cannot modify the thickness. You can select between the thin shell
								and thick shell formulations. | 
						
							| Surface Geometry | The program assigns a zero
								thickness by default. You can modify the thickness of shell in the
									 PropertyManager. You can also select
								between the thin and thick shell formulations. | 
					
 As a general guideline, thin shells can be used when the thickness
				to span ratio is less than 0.05. 
		Applying Loads, Fixtures, and Mesh Controls 
			
			
						
							| Sheet Metal | The loads and fixtures are
								automatically transferred to the mid-surface. 
									To apply a fixture or a load or mesh control
										to a shell edge, select the associated face of the solid. To apply a fixture, load, or mesh control to
										shell vertex, select the associated edge of the solid.  | 
						
							| Surface Geometry | 
									Apply load or fixture to the edges and/or
										vertices of the surfaces. You can apply pressure to a shell edge. The
										pressure is specified per unit area. The program internally
										uses the thickness of the shell. The equivalent force
										applied to the edge is equal to the pressure value times the
										length of the edge times the thickness of the shell.  Since shell elements have rotational
											degrees of freedom, you must differentiate between the
												Immovable (no
											translation) and the Fixed
												Geometry (no translation and no
											rotation) options. You can also apply concentrated
											moments using the Force/Torque PropertyManager.
										 | 
					
Meshing
Apply the
				desired mesh control on the appropriate faces, edges, and vertices. Before meshing,
				verify the active meshing options, and specify all desired mesh controls.
When editing a shell, you can select thin or thick shell
				formulation. Thin shells can be used when the thickness to span ratio is equal to or
				less than 0.05. 
T-Shaped and
					Intersecting Shells 
While it is possible to
				orient shells on sheet metals properly, it is not possible to do so for T-shaped and
				intersecting shells. In such cases, some edges will have mis-aligned elements. As a
				result, nodal stresses are not correct along these edges. We recommend to display
				elemental stresses for such models since no cross-element averaging is
				involved.
Example
						
							|  |  | 
						
							| T-shaped model | Shell meshing of the model | 
						
							|  | 
						
							| Shell meshing of
								T-shaped models always generates shells that cannot be consistently
								aligned. | 
					
After creating a shell mesh, observe the orientation of the top and bottom shell
			faces and display the shell thickness for better visualization. Shell bottom faces have
			orange color. You may need to flip the shell elements to align the shells with the
			required orientation. Select a face (or faces) of a shell body and from the 
Mesh shortcut menu, select 
Flip Shell Elements. If you need to remesh the model, the current
			specifications for the top and bottom shell faces are not retained and you may need to
			redefine them after remeshing.
Viewing Stress Results for Shells 
			
			When listing or plotting stress results, you can select one of the
				following options: 
			
						
							| Top | Total (membrane + bending)
								stresses on the top face | 
						
							| Bottom | Total (membrane + bending)
								stresses on the bottom face | 
						
							| Membrane | Membrane stress component | 
						
							| Bending | Bending stress component | 
					
Refer to the Viewing Results section for more details. 
			 Although displacement results in static studies and temperature
				results in thermal studies do not change if the shells are not aligned, it is
				recommended to align the shells for all studies. In , click Automatic shell surface
					re-alignment to automatically realign the shell surfaces.