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(Established under
section 3 of UGC Act,1956)
Course & Branch :B.E – AERO Max. Marks:80
Title of the Paper :Computer Aided Design and Analysis
Sub. Code :SAEX1033(2010) Time : 3 Hours
Date :13/05/2014 Session
:AN
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PART -
A (10 x 2 = 20)
Answer ALL the Questions
1. Define wireframe and surface model.
2. Differentiate CSG and B-rep.
3. Define rotation. Give the importance of
pivot point.
4. What do you understand by concatenation?
5. Write the limitations of feature technology
in CAD.
6. In
your view, what are the two most-vital reasons the CAD data exchange standards
have been developed?
7. Write the shape function for 1D, 2 noded
linear bar element.
8. Are nodal point and Node distinct? Justify
each if distinct?
9. Write
the functions of Preprocessor.
10. List
the Hardware requirements of Pre and Post processor.
PART – B (5
x 12 = 60)
Answer All the Questions
11. (a) What is geometric modeling? Compare and
contrast the various modeling techniques. (5)
(b)
How are solid modelers categorized? Explain the generic architecture of any
solid modeler. Name some popular solid modelers. (7)
(or)
12. (a)
What is CAD and what are its applications and benefits?
(b)
What are the hardware requirements of a CAD workstation? Explain.
13. What is transformation of
geometry? With suitable figure and matrix discuss following transformation:
(i) Scaling (ii) Reflection (iii) Rotation
(or)
14. Explain
the three types of coordinate systems used to input, store and display model
geometry and graphics.
15. Explain
the salient features of any two modeling package that are being currently used
in the aircraft industry. Which factors influence the selection of a particular
package?
(or)
16. How
feature technology is being initiated in a CAD system? Explain about the
classification of features and its design. State its applications in aircraft
structures.
17. Derive
an expression for stiffness matrix of one dimensional truss element.
(or)
18. Determine
the support reaction R1 and R 3 for stepped bar shown in figure
P1 = 60 kN, P2 = 75
kN
E1 = E2
= E3 = 200 GPa
A1= 24 cm2,
A2= 12 cm2, A3 = 7 cm2
1 GPa = 109 N/m2
19. Derive
the shape function for the constant strain triangular element (CST).
(or)
20. What
are the capabilities of a typical general purpose FEA Package? Enumerate
various type of design problem that could be handled by FEA.
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