Post on 28-Mar-2018
CompoSIDE | Open Academy
Webinar 2 - Composite Shell Design 14/04/2015
Radek Michalik (Managing Director) & Aleksandra Dziekonska (Technical Support)
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O b j e c t i ve s
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Present CompoSIDE design capabilities
Show practical examples of shell structure design in CompoSIDE
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A ge n d a
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Why CompoSIDE ?
Introduction to FESpace
CompoSIDE Modules/Workflows
Practical Design Examples (Live Demo)
CompoSIDE Capabilities - Project Examples
Q&A
Why CompoSIDE?
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F ro m S ke t c h t o D e t a i l e d P ro d u c t D e s i g n …
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???
W hy C o m p o S I D E ?
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W hy C o m p o S I D E #1
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Collaboration &
Integration
W hy C o m p o S I D E ? #2
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Composites Focused
W hy C o m p o S I D E ? #3
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Centralized Data Management
W hy C o m p o S I D E ? #4
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Agile Workflows
W hy C o m p o S I D E ? #5
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Automated Documentation
W hy C o m p o S I D E ? #6
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Flexible Licensing
Introduction to FESpace
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LAMINASpace
FESpace
BOMGen
REPORTSpace CMDB
F E S p a c e I n t ro d u c t i o n
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FESpace interface
Capabilities intro based on shell buckling example
D e s i g n o f S h e l l s - B u c k l i n g C h e c k
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Curved Shell buckling check & iteration
Shell Geometry
Parameters Units Value
Length [mm] 3000
Radius [mm] 2000
Width [mm] 800
Buckling Results Summary
What happened?
F E S p a c e - Re s u l t s
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Model BLF
Critical Strains
[%]
Critical Load
[N/mm] Critical
Load [kN] Weight
[Kg]
Model 1 – (Baseline) 0.38 0.125% 3057.5 2246 80.68
Model 2 – (Base+Tapes) 0.40 0.132% 3781.6 2800 86.54
Buckling Load Factor BLF
Shell Thickness t [mm]
Base (Model 1) 0.38 19.66
Base+ Tapes (model 2) 0.40 22.84
BLF2/BLF1 1.053
(t2/t1)^1/3 1.051
CompoSIDE Modules/Workflows
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C o m p o S I D E M o d u l e s / Wo r k f l o ws
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PROJECTSpace
CMDB
LAMINASpace
FESpace
BOMGen
REPORTSpace
Downstream Design
Upstream Modifications
Live Design Demo
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Composites Plate Design
D e s i g n B r i e f – F l a t Pa n e l D e s i g n ( 1 )
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Design composite plate to meet the design criteria:
Parameters Units Value
LOADS /SF
Working Pressure [MPa] 0.05
Ultimate Load Partial Safety Factor [-] 2.7
Boundary Conditions / Edge Support All edges simply
Supported
Plate Geometry
Length [mm] 3000
Width [mm] 900
Max Thickness [mm] 40 Design Targets
Max. Weight [kg] 25
Max. Material Cost [€/m^2] 250
Max. Working Deflection [mm] 10
Min. Natural Frequency above [Hz] 100
P R OJ E C T S p a c e / C M D B
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PROJECTSpace
CMDB
LAMINASpace
FESpace
BOMGen
REPORTSpace
M a t e r i a l S e l e c t i o n
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L A M I N A S p a c e
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PROJECTSpace
CMDB
LAMINASpace
FESpace
BOMGen
REPORTSpace
P re l i m i n a r y D e s i g n i n L A M I N A S p a c e
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Max. Working Loads (1st Principle)
Shear Force (Qy) 22 [N/mm]
Bending Moment (My) 5060 [Nmm/mm]
Sandwich Laminate
¤ Pre-preg/PVC foam
Strip Beam approximation
¤ Working Loads:
Verification:
¤ Strength (Ultimate Load)
• Fibre Failure /Core Shear
¤ Local Stability (Wrinkling)
Qy
Qy
Mymax
F E S p a c e
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CMDB
PROJECTSpace
LAMINASpace
FESpace
BOMGen
REPORTSpace
F E M o d e l C re a t i o n - P l a t e
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B O M G e n
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PROJECTSpace
CMDB
LAMINASpace
FESpace
BOMGen
REPORTSpace
B i l l o f M a t e r i a l G e n e ra t i o n
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R E P O R T S p a c e
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PROJECTSpace
CMDB
LAMINASpace
FESpace
BOMGen
REPORTSpace
B o M Re p o r t G e n e ra t i o n
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D e s i g n S u m m a r y
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CMDB
PROJECTSpace
LAMINASpace
FESpace
BOMGen
REPORTSpace
Panel Design Results
F E S p a c e – Re s u l t s S u m m a r y
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Fibre Failure RF Core Failure RF
D e s i g n C o st Tra n s p a re n c y
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Flat Panel Design CU Summary CU
LAMINASpace - Included in Subscription
FESpace - Static Run 16 2 iterations & 2 load cases
FESpace - Failure 3 1 iterations & 1 load case
BOM Creation 25 One off (updates free)
Laminates Table Export for CAD 6 For one component
BoM Report Generation 25
Total CompoSIDE Units (CU) 75
Approximate Cost (€) € 7.5 CU’s cost: € 0.1 (CU-8000 Plan)
G e t s t a r t e d !
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Sign up for 30 days free trial!!
¤ CU-1000 Recommended for low monthly use of FESpace
¤ CU-8000 Recommended for heavy FESpace Users
Project Examples
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Shell Design Examples
C o m p o s i t e B r i d ge – S h e l l D e s i g n
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Bridge Geometry and Load Case Visualization
Bridge Deformation
C o m p o s i t e B r i d ge
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Internal Forces (In-Plane)
Modal Analysis – 1st Mode
P re s s u re Ve s s e l D e s i g n
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Geometry (1/8th)
Boundary Conditions and Loading
P re s s u re Ve s s e l D e s i g n
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Total Deformation
O t h e r S h e l l D e s i g n E xa m p l e s
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Extruded Airfoil – Wing Panel
L-Flange Beam - Twisting
Shells with Cut-outs and beam elements
Questions & Answers
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S u p p o r t & Tra i n i n g
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Support
FAQs
CompoSIDE Tutorials
Webinars
Knowledge Base
www.composide.com/support-and-training
N e e d H e l p ?
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Email: support@composide.com
Support & Knowledge Base Portal
Support Chat
Technical Documentation TechDocs
YouTube Channel Tutorials
G e t s t a r t e d !
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Sign up for 30 days free trial!!
Thank you
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