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Stress Analysis Report
| Analyzed File: | FEA_AI_Plate.ipt |
| Autodesk Inventor Version: | 2025 (Build 290162000, 162) |
| Creation Date: | 8/18/2024, 6:43 PM |
| Study Author: | BRG |
| Summary: |
Static Analysis:1
General objective and settings:
Design Objective Single Point Study Type Static Analysis Last Modification Date 8/18/2024, 1:39 PM Model State [Primary] Detect and Eliminate Rigid Body Modes No iProperties
Summary
Author BRG Project
Part Number FEA_AI_Plate Designer barto Estimated Cost $0.00 Creation Date 12/29/2021 Status
Design State WorkInProgress Physical
Material Aluminum 6061 Density 0.0975437 lbmass/in^3 Mass 0.281858 lbmass Area 27.7055 in^2 Volume 2.88955 in^3 Center of Gravity x=0.00000000000149869 in
y=0 in
z=0.125 inNote: Physical values could be different from Physical values used by FEA reported below.
Mesh settings:
Avg. Element Size (fraction of model diameter) 0.05 Min. Element Size (fraction of avg. size) 0.2 Grading Factor 1.5 Max. Turn Angle 60 deg Create Curved Mesh Elements Yes Material(s)
Name Aluminum 6061 General Mass Density 0.0975437 lbmass/in^3 Yield Strength 39885.4 psi Ultimate Tensile Strength 44961.7 psi Stress Young's Modulus 9993.1 ksi Poisson's Ratio 0.33 ul Shear Modulus 3756.8 ksi Part Name(s) FEA_AI_Plate.ipt Operating conditions
Force:1
Load Type Force Magnitude 300.000 lbforce Vector X 300.000 lbforce Vector Y 0.000 lbforce Vector Z 0.000 lbforce Selected Face(s)
Fixed Constraint:1
Constraint Type Fixed Constraint Selected Face(s)
Results
Reaction Force and Moment on Constraints
Constraint Name Reaction Force Reaction Moment Magnitude Component (X,Y,Z) Magnitude Component (X,Y,Z) Fixed Constraint:1 300 lbforce -300 lbforce 0 lbforce ft 0 lbforce ft 0 lbforce 0 lbforce ft 0 lbforce 0 lbforce ft Result Summary
Name Minimum Maximum Volume 2.88955 in^3 Mass 0.281858 lbmass Von Mises Stress 0.0245998 ksi 2.19813 ksi 1st Principal Stress -0.0294238 ksi 2.22788 ksi 3rd Principal Stress -0.876307 ksi 0.268637 ksi Displacement 0 in 0.000405761 in Safety Factor 15 ul 15 ul Stress XX -0.0923591 ksi 2.22788 ksi Stress XY -0.609441 ksi 0.607612 ksi Stress XZ -0.126426 ksi 0.122485 ksi Stress YY -0.876307 ksi 0.37586 ksi Stress YZ -0.0352037 ksi 0.0351695 ksi Stress ZZ -0.064454 ksi 0.379174 ksi X Displacement 0 in 0.00040527 in Y Displacement -0.0000477288 in 0.0000477212 in Z Displacement -0.0000082776 in 0.00000905415 in Equivalent Strain 0.000002427 ul 0.00019846 ul 1st Principal Strain 0.000000695678 ul 0.000220938 ul 3rd Principal Strain -0.0000861438 ul -0.00000000364206 ul Strain XX -0.000000591293 ul 0.000220938 ul Strain XY -0.0000811116 ul 0.0000808683 ul Strain XZ -0.0000168262 ul 0.0000163017 ul Strain YY -0.0000861438 ul 0.0000193095 ul Strain YZ -0.00000468533 ul 0.00000468077 ul Strain ZZ -0.0000704016 ul 0.0000257237 ul Figures
Von Mises Stress
1st Principal Stress
3rd Principal Stress
Displacement
Safety Factor
Stress XX
Stress XY
Stress XZ
Stress YY
Stress YZ
Stress ZZ
X Displacement
Y Displacement
Z Displacement
Equivalent Strain
1st Principal Strain
3rd Principal Strain
Strain XX
Strain XY
Strain XZ
Strain YY
Strain YZ
Strain ZZ
Static Analysis:2
General objective and settings:
Design Objective Single Point Study Type Static Analysis Last Modification Date 8/18/2024, 2:12 PM Model State [Primary] Detect and Eliminate Rigid Body Modes No iProperties
Summary
Author barto Project
Part Number FEA_AI_Plate Designer barto Estimated Cost $0.00 Creation Date 12/29/2021 Status
Design State WorkInProgress Physical
Material Aluminum 6061 Density 0.0975437 lbmass/in^3 Mass 0.281858 lbmass Area 27.7055 in^2 Volume 2.88955 in^3 Center of Gravity x=0.00000000000149869 in
y=0 in
z=0.125 inNote: Physical values could be different from Physical values used by FEA reported below.
Mesh settings:
Avg. Element Size (fraction of model diameter) 0.05 Min. Element Size (fraction of avg. size) 0.2 Grading Factor 1.5 Max. Turn Angle 60 deg Create Curved Mesh Elements Yes Material(s)
Name Aluminum 6061 General Mass Density 0.0975437 lbmass/in^3 Yield Strength 39885.4 psi Ultimate Tensile Strength 44961.7 psi Stress Young's Modulus 9993.1 ksi Poisson's Ratio 0.33 ul Shear Modulus 3756.8 ksi Part Name(s) FEA_AI_Plate.ipt Operating conditions
Force:1
Load Type Force Magnitude 300.000 lbforce Vector X 300.000 lbforce Vector Y 0.000 lbforce Vector Z 0.000 lbforce Selected Face(s)
Fixed Constraint:1
Constraint Type Fixed Constraint Selected Face(s)
Results
Reaction Force and Moment on Constraints
Constraint Name Reaction Force Reaction Moment Magnitude Component (X,Y,Z) Magnitude Component (X,Y,Z) Fixed Constraint:1 300 lbforce -300 lbforce 0 lbforce ft 0 lbforce ft 0 lbforce 0 lbforce ft 0 lbforce 0 lbforce ft Result Summary
Name Minimum Maximum Volume 2.88955 in^3 Mass 0.281858 lbmass Von Mises Stress 0.0245971 ksi 2.19813 ksi 1st Principal Stress -0.0294222 ksi 2.22788 ksi 3rd Principal Stress -0.876306 ksi 0.268637 ksi Displacement 0 in 0.000405761 in Safety Factor 15 ul 15 ul Stress XX -0.0923566 ksi 2.22788 ksi Stress XY -0.609443 ksi 0.607612 ksi Stress XZ -0.126426 ksi 0.122485 ksi Stress YY -0.876306 ksi 0.375859 ksi Stress YZ -0.0352037 ksi 0.0351695 ksi Stress ZZ -0.064454 ksi 0.379174 ksi X Displacement 0 in 0.00040527 in Y Displacement -0.0000477288 in 0.0000477212 in Z Displacement -0.00000827755 in 0.0000090542 in Equivalent Strain 0.000002427 ul 0.00019846 ul 1st Principal Strain 0.000000695348 ul 0.000220938 ul 3rd Principal Strain -0.000086144 ul -0.00000000364264 ul Strain XX -0.000000591635 ul 0.000220938 ul Strain XY -0.0000811119 ul 0.0000808682 ul Strain XZ -0.0000168262 ul 0.0000163017 ul Strain YY -0.0000861439 ul 0.0000193095 ul Strain YZ -0.00000468532 ul 0.00000468077 ul Strain ZZ -0.0000704009 ul 0.0000257236 ul Figures
Von Mises Stress
1st Principal Stress
3rd Principal Stress
Displacement
Safety Factor
Stress XX
Stress XY
Stress XZ
Stress YY
Stress YZ
Stress ZZ
X Displacement
Y Displacement
Z Displacement
Equivalent Strain
1st Principal Strain
3rd Principal Strain
Strain XX
Strain XY
Strain XZ
Strain YY
Strain YZ
Strain ZZ
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