Light-weight Composite Beam Design
 
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Description:

Purpose of calculation:
Consider a cantilever beam with a load applied at the free end. The applied load creates a bending moment which is a maximum at the fixed end, and a shear force along the length of the beam. In a sandwich panel these forces create tension in the upper skin and compression in the lower skin. The core spaces the facing skins and transfers shear between them to make the composite panel work as a homogeneous structure.
Calculation Reference
HexWeb SANDWICH DESIGN MANUAL

Calculation Validation
Reproduced result published in manual.

Calculation Procedure

The following face materials can be selected using a drop down combo box (you could also add your own).

• Epoxy UD CARBON tape (0°) 60% volume fraction
• Epoxy UD GLASS tape (0°) 55% volume fraction
• Epoxy WOVEN CARBON (G793-5HS) 55% volume fraction
• Epoxy WOVEN ARAMID (285K-4HS) 60% volume fraction
• Epoxy WOVEN GLASS (7781-8HS) 50% volume fraction
• Phenolic WOVEN GLASS (7781-8HS) 55% volume fraction
• ALUMINIUM Alloy 2024 T3
• ALUMINIUM Alloy 5251 H24
• ALUMINIUM Alloy 6061 T6
• STEEL carbon 1006
• STEEL carbon 1017
• Exterior PLYWOOD Fir
• Tempered HARDWOOD Teak

The following core materials can be selected using a drop down combo box (you could also add your own).

• 3003 Aluminium  29kg/m³
• 3003 Aluminium  37kg/m³
• 3003 Aluminium  42kg/m³
• 3003 Aluminium  54kg/m³
• 3003 Aluminium  59kg/m³
• 3003 Aluminium  83kg/m³
• 5052 Aluminium  37kg/m³
• 5052 Aluminium  50kg/m³
• 5052 Aluminium  54kg/m³
• 5052 Aluminium  72kg/m³
• 5052 Aluminium  83kg/m³
• 5052 Aluminium  127kg/m³
• 5052 Aluminium  130kg/m³
• 5056 Aluminium  37kg/m³
• 5056 Aluminium  50kg/m³
• 5056 Aluminium  50kg/m³
• 5056 Aluminium  72kg/m³
• HRH10 Nomex (Aramid) 29kg/m³
• HRH10 Nomex (Aramid) 32kg/m³
• HRH10 Nomex (Aramid) 32kg/m³
• HRH10 Nomex (Aramid) 48kg/m³
• HRH10 Nomex (Aramid) 48kg/m³
• HRH10 Nomex (Aramid) 64kg/m³
• HRH10 Nomex (Aramid) 64kg/m³
• HRH10 Nomex (Aramid) 80kg/m³
• HRH10 Nomex (Aramid) 96kg/m³
• HRH10 Nomex (Aramid) 123kg/m³
• HRH10 Nomex (Aramid) 144kg/m³

1) Determine Panel Properties

• Thickness of face material and core
• Young's modulus of face and core
• Shear modulus of core
• Core allowable shear stress
• Core Cell size
• Poisson's ratio of face
• Limiting stress in face
• Safety Factor
• Poisson's ratio term
• Distance between face centres
• Critical intracell buckling stress
• Critical face wrinkling stress
• Allowable Tensile Stress on Face
• Panel stiffness coefficient

2) Beam Loading Assessment. The following beam loading conditions can be selected using a drop down combo box:

L1) Simple Support with Uniform Load Distribution
L2) Both Ends Fixed with Uniform Load Distribution
L3) Simple Support with Central Load
L4) Both Ends Fixed with Central Load
L5) Cantilever with Uniform Load Distribution
L6) Cantilever with Load at End
L7) Cantilever with Triangular Load Distribution

• Dimensions of panel
• max shear coefficient
• max bending moment coefficient
• bending deflection coefficient
• shear deflection coefficient
• Total load on beam
• Max bending moment
• Max face stress
• Max shear force
• Core shear stress
• Bending deflection
• Shear deflection
• Total deflection

3) Equivalent plate properties for use with finite element software
It is possible to use the following equivalent plate element properties to match stress and deflection with standard plate elements using finite element analysis software. This should only be done if you can assure that the following conditions are true:
Shear deflections are negligible compared to bending deflections.
Strength of core material is independently checked.

• Equivalent plate thickness for plate element.
• Equivalent Young's modulus
• Check deflection (note that only deflection due to bending is calculated)

Calculation Reference
Composites Design
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Composite Materials
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Composite structures
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Submitted On:

03 Mar 2010

Submitted By:

JohnDoyle

File Date:

19 Feb 2010

File Version:

1.1

File Size:

188.44 Kb

File Type:

xlsx

Downloads:

17

Rating:

Total Votes:3

Comments:

Esmat 2010-02-10 11:03:20 Very good approach