ollowing Paper ID and Roll No. to be filled in your Answer Book) Roll No.
B. Tech. ( E~. III) ODD SEMESTER THEORY
EXAMINATION 2010-11 THERMAL ENGINEERING
_·ote:- (1) Attempt all questions. (2) Assume missing data suitably, if any.
)
. . initially at 75 kPa pressure, 1000 K temp and 1.2 m3 'olume, first compressed
isothermally
till its volume
.. mes half of the initial volume then further compressed - onstant pressure till its volume becomes half of the 'olume before constant pressure compression. And then
)
:c
to its original state following polytropic process.
F'
'work transfer and heat transfer during each process.
(i)
Write Kelvin-Planck
and Clausius statements
of
second law of thermodynamics. (ii)
A fluid undergoes a reversible adiabatic compression from 0.5 MPa, 0.2 m3 to 0.05 m3 according to law pvu
=
constant. Determine the change in enthalpy,
internal energy, entropy and work transfer during the process.
(c)
Write short notes on : (i)
Thennodynamic system
(ii)
Concept of continuum
(iii) Camot theorem. 2.
Attempt any two parts ofthe following: (a)
What are the assumptions made in the air standard cyCles ? Show the Otto, Brayton and dual c cle on P-v and T-s diagram.
(b)
(i)
For the same compression ratio and heat rejection,' which cycle is more efficient: Otto or Diesel? Explain with the help of P-v and T-s diagrams.
(ii) (c)
Explain the effect of pressure ratio on the net work output and efficiency of Brayton c Ie.
What do you understand by multi stage compression ? What are its importance over single stage ompression? Obtain the condition for optimum pressure ratio for perfect intercooling in between two stages of compression, ifthe inlet and outlet pressure are PI and P3.
3.
Attempt any two parts of the following: (a)
(lOx2=20)
(i)
What do you understand by triple point and critical point? Show it on T-s diagram and write the value of pressure and temperature of water at critical point.
(ii)
Show Rankine cycle on P-v, T-s and H-s diagram._. How superheating improves the efficiency of rankine cycle?
(b)
What do you understand by choking in nozzle flows ? Discuss
the effect of area change
supersonic flow.
in subsonic
and
· Compare turbojet engine =: es.
~
_0
°
=: o. simple vapoureompression ea: schematic and also show the
1 temperature, dry bulb temperature 'di . erstand by heat pump? Show that of heat pump and refrigerator can
insulated small diameter wire has a carrying capacity than an uninsulated
(::...
::' crass and steel, each of thickness 1 em, are macI. The outer surface of brass is kept c:::~00 :::C ~:
d the outer surface of steel is kept at O°C. em perature of common interface?
The
nductivities of brass and steel are in the
(b)
Define effectiveness and NTU of a Heat exchanger. Derive the expression for effectiveness
for counter flow heat
exchanger. (c)
What is Prandtl
and Nusselt
number?
Write the
expressions ofNusselt number for laminar and turbulent flow over a flat plate.
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