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West Bengal Institute of Technology (WBIT) 2008-2nd Sem B.Tech Computer Science and Engineering Computer Science - Thermodynamics & Fluid Mechanics - Question Paper

Wednesday, 17 July 2013 06:15Web



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" INGIFTBE-IKH J & MANAGEMENT EXAMINAT' O l    - 2008

MECHANICAL SCW&C A

SEMESTER -2

I Full Marks : 70

Time : 3 Hours )


GROUP - A (M ultiple Choice Type Questions}

10 x 1 * 10


C hjcse the ccn'ccc alternatives for the following :

ij Which Ci tiiC follow mg is an intensive thermodyn. or u property ?

a) VtivuTja    b) Temperature

c) M;:ss    d) Energy.

ii) For i ;i lii cv. rsible process, change in entropy is

a} greater than dQ/T    b) less than dQ/T

c) zero    d) equal to cQ/T,

ill) Durii;g ihrouiing, which of the following quantity dec... not change ?

a) Internal energy    b) Entrc-jy

c) Prussia e    d) Enthalpy

iv)


Woi k di aic in a free expansion is .

a) Positive    b) Negatm*

c) Zero    d) Maxa.-Um.

A cycle v/ith constant volume heat addition and constant volume heat rejectic i is

v)


Diesel cycle


vl)


b)

c)

d)


b)

c) Joule cycle    d) Rankuie cycle,

Triple point of a pure substance is a point at which a) liquid and vapour coexist so: id and vapour coexist dOiid u.a liquid coexist all tiixee phases coexist.


a) , Otio vycle


H-222833 (3)

vii) BanouL s equation deals with the conservation of

* : ' '    * ' ' * -VI    -

Ci Energy    ;d) Work,

C jntinuity aquation is based on the principle of conservation of 4 Mass    b) Momentum

o) Energy    , d)

' o     *     * ? A .     -

A. Pitot tube is used for measuring

'            ..    v ..v.4 i :    A.I.' .

tj rStacc: of fluid    a)

c) Density 6f fluid    d)

Dynamic viscosity has dimensions of

a) MWf2    *?)

c) ML1T-2    ti)


GROUP - a ( Short Answer Type Qutetim* ) Answer any three of the followin '.


vtL


r


Entropy.

VelcMy offtuid Viscosity of fluid.


c :2 j.


iT-i


M- i L- i T-i.


3 Y


2,    Statw the first law of thermodynamics for a closed system undergoing e cycL 15

' p-i'ccess..    .    .,    .    .     .

3,    l&rplain thrmodynunic eqi

4,    riic fluid flow is given by V= x2 yi + y 2z - ( 2 xyz + yz 2 ) k. Show that tliis 3 a > oi possible steady incompressible flow. Calculate ilie velocity ano acceltr x lo*.

1 2, 1, 3 ).        

5,    Di'&w a block digram of vapour compression xeirigeration cycle and also l: c v to responding P-V and T-S plots.

b. D .iive B raoullis equation form first priiicipies, stating ti e assumptions.

V. ii plain PMl1-1 and PMM-2.

ffe-iSL J83 (til    .

GROUP-C (Long Answer Type Questions)

Answer any three of the following,    3 x 15 - *5

8. a) Which is a more effective way of increasing the efUciency of a Carnot engine to increase source temperatue ( T y ), keeping sins temperature ( T% ) constant or

to decrease T2 keeping Tr constant.

b)    State Clausius inequality.

c)    A mass of m kg of liquid ( specific heat * Cp) at a temperature T j is mixed with an equai iwuss of the same liquid at a temperature T2 ( Tj > Tu ) and the system is thermally insulated. Show that the entropy charge of th-.i vaJverse is given by

i , + T o 2mC I i --1

p pf T

\ 1 1 1 2 )


and prove that this is necessarily positive.    3 + 2 + 10

9.    a) Derive the expression for efficiency of an Otto cycle and show the process on

p-V and T-s planes.

b)    For the same compression ratio, explain why the efficiency of Otto cycle is greater than that of Diesel cycle.

c)    In a diesai engine the compression ratio is 13 : 1 and fuel is cut off at 8% of f h stroke. Find the air standard efficiency of the engine. Take y for ir 1.4

.    . 5 + 3 + 2 + 5

10.    a) A gas occupies 0.024 m3 at 700 kPa and 95C, Ic is expanded in the non-flow

process according to the law pv 12 = constant to a pressure of 70 kPa after which it is heated at a constant pressure back to its original temperature. Sketch the process on the p-V and T-s diagrams and calculate for the whole process the work done and the heat transferred. Take Cp =1.047 and C u = 0.775 kJ/kg K for the gas.

b) A rigici closed tank of volume 3m3 contains 5 kg of wet l e un at a pressure oS 200 kPa The tank is heated until the steam become* dry saturated. Determine the pressure and the heat transfer to the tank.    8 t 7

C8/B T A/8 JL i/ME-201/08    6

' \ .


11.    it) Write the steady flow eni&rgyySLWon for a singlfc ateam entering and sUgie

sUaia-leaving a control    tae varum terms.

h) ;vt the inlet to a nozzle, C5, enthalpy c: t.e ;lujd pacing is 3000 kJ/tg .uva velocity is 60 m/s. At the exit, the euiaalpy is 2762 teJ/kg. The m/iz-I- ti ho/teontal andthereis negligible heatlos

I) Find the velocity at tMfe nozzle exit

ii) The inlet area is 0.1 m 2 aind the siieciflc volume tit inle H 187 if. Find the mass flow rate.    '    ,

ill) If the specific volume at the nozzle exit is 0.498 m 3/kg, find :: *> e-nt urge, of the nozzle.    

12.    u) Derive Euler's equation, of motion along a gtreamliae

b) A venturimeter has inlet sund throat diameters of 300 mm and 150 nnr. V /.-flows through it at the rate of O.Q65ni3/ and the differential gauge is defies.. by 1.2 m. The specific gravity of the ra&iiometric liquid is 1.6. Determine ih*; coefficient of discharge of the venturimeter.

o) A Jet of water from a 25 mm diameter nozzle is directed vertically upw rds Assuming that the jet remains circular Sind neglecting any loss of energy, wlu will be the diameter of the jet at a point 4.5 m above the nozzle, if the jet U \

&e nozzle with a velocity of 12 m/s ?' ;    5 t :'* y

13.    a) A circular disk of diameter d is slowvy rotated la a liquid of viscosity at a n'iu

distance h from a fixed surface. Derive an expression for the lorqu necessary to maintain an angular velocity a),

b) Distinguish between the follow :

laminar and turbulent flow

4


it)    compressible and incompressible fluid

ia)    static pressure and stagnation pressure

iv)    viscous and inviscid fluid,    7 + 3

14, Write short notes on any three of the following :    3x5

a)    Pitot tube ,    *

L]    Orifice meter

c)    Point function and path function

aj    S-reamline. streakline and pathline.

END    :

(jt'32?3i3 W\    K







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