1. Draw TOP and LEFT SIDE VIEW
of the object shown.
2. Define isotropic
materials and homogeneous materials, give an example of each.
3. Define Boundary
layer. Draw a sketch showing different boundary-layer flow regimes on a flat
plate.
5. Water flows at 8
kg/s through a diffuser with A1=7×10-4 m2 and
A2=4×10-3 m2. Determine the
increase in static pressure between section 1 and section 2. Assume
frictionless flow and water density 1000 kg/m3.
6. An elastic bar of
cross section A and length L is held fixed at both ends. The bar has modulus of
elasticity E and coefficient of thermal expansion α. Derive the expression for
axial force due to temperature increase of ΔT. (Assume no buckling of the bar).
7. For the plane
stress shown in the stress element, draw the Mohr’s circle to find the maximum
in-plane shearing stress and corresponding normal stress.
8. Construct shear and
bending-moment diagrams showing peak values for the simply supported beam
loaded with the forces shown in figure.
9. Draw the open cycle
gas turbine in simple block diagram form and show the corresponding processes
on a T-S plane.
10. What is cavitation? List any two
problems caused by caviations in turbines.
11. Compute the pressure drop when water
flows at 3 liter/s through a steel pipe with diameter 50 mm and 40 m length.
Assume, density of water 1000 kg/m3 and friction factor f=0.02.
12. A composite wall of two 0.5 m thick
layers has a temperature 150ºC on one face and 10ºC on the other face. Thermal
conductivity of Layer-1 is k1=0.05 W/m-K and Layer-2 is k2=0.5
W/m-K.
Consider face area A1=A2=2 m2. What is
the combined thermal resistance of the wall? Find the heat transfer per unit
surface area.
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