same bk_with direct time dependent loading condition with results but the approach is deferent from the industry.

1. CAD model
verification of a
simple bracket
sheet metal model
•Objective
•Cad model
•Manufacturing sheet.
•Fea model
•Basic analysis
methods implemented.
•Loading condition with
respect to the analysis
methods.
•Material and property
•The results
•conclusion

2. objective
To do some thing “”FTP””
To verify the analytical skills with the help of
CAD/CAE tool and also with the microsoft tool.
To verify the tool knowledge to achieve the goal.

3. The CAD model

4. Manufacturing model
• 2.5mm sheet with aluminum alloy • 2.5mm sheet with aluminum alloy

5. Outer face with offseted FEA
model

6. Direct Transient analysis (0-1.6 with
cosine function)
1. Direct transient analysis:-
I. Magnitude and the location are
same as static analysis with a
function of cosine with phase 250
and time range is 0.0 to 1.6.
II. Boundary condition is same as
static analysis.

7. Load and boundary
condition in direct
transient response
analysis

8. Load and boundary condition for
static x-directional loading

9. Load and boundary condition for
static y-directional loading

10. Load and boundary condition for
static Z-directional loading

11. Load and boundary condition for
direct transient x,y,z-directional
loading
Load as per static with time
Full constrained area
function

12. Material selected for
the component and its
Engineering property
for analysis

13. Material and property
• Aluminum alloy with SI unit
YOUNGS
SHEAR MODULUS POISIONS RATIO DENSITY YIELD_STRESS_VALUE
MODULUS
7.00E+04 2.632E+04 0.33 2.80E-09 3.50E+04

14. Analysis results
• Transient (direct ) analysis result
• X-directional load case
• Spc-force & External force
• Max- displacement and vonmises stress value and
region plot
• y-directional load case
• Spc-force & External force
• Max- displacement and vonmises stress value and
region plot
• z-directional load case
• Spc-force & External force
• Max- displacement and vonmises stress value and
region plot

15. X-directional load case
Direct transient response
analysis results

16. Reaction force and external force result in direct
transient response analysis for x-directional
loading
Spc- force External force

17. x-directional load-case
Max displacement result Max vonmises stress result

18. Maximum value of Results corresponding to
time in x-direction
X-DIRECTIONAL DYNAMIC_LOAD(0-1.6)
DISPLACEMENT(MAX)(Node-8266,7096)
time 0.266667 1.333333 1.599999
VALUE 1.62E+00 1.62E+00 1.82E+00
vonmises stress(max) Nodal_results
elements 10819/10845/10818/10847
NODE 5836
TIME 0.266667 1.333333 1.599999
VALUE 3.17E+02 3.17E+02 3.37E+02
elements 8995/9024/8996/9022
NODE 5786
TIME 0.266667 1.333333 1.599999
VALUE 3.17E+02 3.17E+02 3.37E+02

19. Y-directional load case
Direct transient response
analysis results

20. Reaction force and external force result in direct
transient response analysis for y-directional
loading
Spc- force External force

21. y-directional load-case
Max displacement result Max vonmises stress result

22. Maximum value of Results corresponding to
time in y-direction
Y-DIRECTIONAL DYNAMIC_LOAD(0-1.6)
DISPLACEMENT(MAX)(NODE-184,7212)
time 0.266667 1.333333 1.599999
VALUE 1.27E+00 1.27E+00 1.42E+00
vonmises stress(max) Nodal_results
elements 8994/8995/9026/9024
NODE 5787
TIME 0.266667 1.333333 1.599999
VALUE 2.62E+02 2.62E+02 2.93E+02
elements 10818/10847/10817/10849
NODE 7837
TIME 0.266667 1.333333 1.599999
VALUE 2.62E+02 2.62E+02 2.93E+02

23. Z-directional load case
Direct transient response
analysis results

24. Reaction force and external force result in direct
transient response for z-directional loading
Spc- force External force

25. z-directional load-case
Max displacement result Max vonmises stress result

26. Maximum value of Results corresponding to
time in z-direction
z-DIRECTIONAL DYNAMIC_LOAD(0-1.6)
DISPLACEMENT(MAX)(NODE-7507/5359)
time 0.266667 1.333333 1.599999
VALUE 2.33E+00 2.33E+00 2.62E+00
vonmises stress(max) Nodal_results
elements 10226/10227/10223/10224
NODE 7076
TIME 0.266667 1.333333 1.599999
VALUE 2.93E+02 2.93E+02 3.28E+02
elements 11285/11286/11288/11289
NODE 8250
TIME 0.266667 1.333333 1.599999
VALUE 2.93E+02 2.93E+02 3.28E+02

27. IT HAS
TO BE
FILLED

28. TO BE FILED

29. TO BE FILED

30. CONCLUSION
THIS IS JOST THE BEGINNING
PICTURE ABHI BAKIHE
With thanks,
Manas Ranjan Ray