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WS6-1 PAT302, Workshop 6, December 2004 Copyright2004 MSC.Software Corporation WORKSHOP 6 MID-SURFACE EXTRACTION WING SECTION 3D Parasolid Solids 2D Surfaces

WORKSHOP 6 MID-SURFACE EXTRACTION WING · PDF fileGeneral outline of workshop steps (continued)

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Page 1: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-1PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

WORKSHOP 6

MID-SURFACE EXTRACTIONWING SECTION

3D Parasolid Solids 2D Surfaces

Page 2: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-2PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

Page 3: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-3PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

Problem Description The design department has produced a solid model of an

aircraft wing section.

The task is to extract mid-surfaces from the solid model,preparing for shell meshing.

MID-SURFACEWING SECTION

Page 4: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-4PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

The solid model consists of five individual solids asshown in the exploded view.

MID-SURFACEWING SECTION

Page 5: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-5PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

The model of the wing section is shown without theupper wing skin.

Rib (3)

Rib stiffener (9)

Lower wing skin

Rib cap (6)

MID-SURFACEWING SECTION

Page 6: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-6PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

Idealization Replace the solid geometry with surface geometry. Mesh the surfaces

to create plate elements. Mesh the edges of surfaces to create barelements.

Wing skins and ribsare modeled usingplate elements

Rib stiffeners andrib caps aremodeled usingbar elements

MID-SURFACEWING SECTION

Page 7: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-7PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

General outline of workshop steps Import the Parasolid model file wing_section.xmt_txt

MID-SURFACEWING SECTION

Page 8: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-8PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

Rib Solids, Solid 1:3

Skin Solids, Solid 4:5

General outline of workshop steps (continued) Five parasolid solids

MID-SURFACEWING SECTION

Page 9: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-9PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

Rib321

Solid 3.7Solid 2.7Solid 1.7Offset SolidFace List

Solid 3.5Solid 2.5Solid 1.5Solid FaceList

General outline of workshop steps (continued) Create rib surfaces

They will be the length(X-direction) of the ribs

MID-SURFACEWING SECTION

Page 10: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-10PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

General outline of workshop steps (continued) Create rib stiffener surfaces

They will be the width (Z-direction) of the ribs

Solid3.41

Solid3.37

Solid3.33

Solid2.41

Solid2.37

Solid2.33

Solid1.41

Solid1.37

Solid1.33

OffsetSolidFace

Solid3.40

Solid3.36

Solid3.32

Solid2.40

Solid2.36

Solid2.32

Solid1.40

Solid1.36

Solid1.32

SolidFace

987654321

MID-SURFACEWING SECTION

Page 11: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-11PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

General outline of workshop steps (continued) Created rib and rib stiffener surfaces

MID-SURFACEWING SECTION

Page 12: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-12PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

General outline of workshop steps (continued) Use the manual or automatic mode to extract mid-surfaces from the

wing skin solids. Solid Face List: Solid 4.6 5.6 Offset Solid Face List: Solid 4.1 5.1

MID-SURFACEWING SECTION

Page 13: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-13PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

General outline of workshop steps (continued) There is a gap between the top or bottom of the rib/rib stiffener surfaces

and the wing skin surfaces. It is 0.050 inch which is half of the wing skinthickness.

Wing skin surface

Rib surface

Rib stiffenersurface

Gap

MID-SURFACEWING SECTION

Page 14: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-14PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

General outline of workshop steps (continued) Only simple (green) surfaces can be extended. MSC.Patran will

automatically attempt to convert complex (magenta) surfaces intogreen surfaces before performing the surface extend operation.

In cases where the automatic conversion fails, a manual surface refitmay be required using Geometry: Edit/Surface/Refit.

MID-SURFACEWING SECTION

Page 15: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-15PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

General outline of workshop steps (continued) Extend the rib stiffener surfaces to the wing skin surfaces to eliminate

those gaps. Do not break the wing skin surfaces during the extendoperation.

Extend rib stiffenersurface at both ends

MID-SURFACEWING SECTION

Page 16: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-16PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

General outline of workshop steps (continued) Extend the rib surfaces to the wing skin surfaces to eliminate those

gaps. Do not break the wing skin surfaces during the extend operation.

Extend rib surface atboth top and bottom

MID-SURFACEWING SECTION

Page 17: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-17PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

General outline of workshop steps (continued) Use the rib stiffener surfaces to break the rib surfaces. The rib surface

edges resulting from this operation can be meshed with bar elements torepresent the stiffeners.

Delete the rib stiffener surfaces.

MID-SURFACEWING SECTION

Page 18: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-18PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

General outline of workshop steps (continued) Extend the wing skin surfaces 4.5 inches in the span direction.

Notice that MSC.Patran automatically refits the magenta surfaces to greensurfaces.

Note that the surface extension retains the contour of the surface.

MID-SURFACEWING SECTION

Page 19: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-19PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

General outline of workshop steps (continued) For a further demonstration of the Surface Extend tool, use the extend

by percentage to lengthen the cord of the wing skin by 10% inanticipation of front and rear spars.

MID-SURFACEWING SECTION

Page 20: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-20PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

General outline of workshop steps (continued) Finally associate the upper and lower rib surface edges with the wing

skin surfaces. This will enforce congruent meshes between the ribs andwing skins.

MID-SURFACEWING SECTION

Page 21: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-21PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation

MID-SURFACEWING SECTION

Page 22: WORKSHOP 6 MID-SURFACE EXTRACTION WING  · PDF fileGeneral outline of workshop steps (continued)

WS6-22PAT302, Workshop 6, December 2004Copyright2004 MSC.Software Corporation