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Monday 1 July 2013

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Steel Authority Of India Limited
SAIL Management Trainee
Chemical Engineering Model Papers
Q.1.Loss of heat from unlagged steam pipe to the ambient air is by
  • conduction
  • convection
  • radiation
  • all (a), (b) & (c)
Q.2.Fourier's law applies to the heat transfer by
  • convection
  • radiation
  • conduction
  • all (a), (b) & (c)
Q.3.Fourier's law of heat conduction applies to .......... surfaces.
  • isothermal
  • non-isothermal
  • both (a) and (b)
  • neither (a) and (b)
Q. 4.Unsteady state heat conduction occurs, when
  • temperature distribution is independent of time
  • temperature distribution is dependent on time
  • heat flows in one direction only
  • three dimensional heat flow is concerned
Q.5.What is the unit of thermal conductivity ?
  • Kcal/hr.m2 0C
  • Kcal/hr.m. 0C
  • Kcal/hr.m
  • Kcal/hr.0C
Q.6.The unit of heat transfer co-efficient is
  • BTU/hr.ft2 0F
  • BTU/hr.0F.ft.
  • BTU/hr.0F
  • BTU/hr.ft
Q.7.Which of the following is correct ?
  • Rate = Driving force * Resistance
  • Driving force = Rate * Resistance
  • Resistance = Driving force * Rate
  • Rate = Resistance/Driving force
Q.8.An insulator should have
  • low thermal conductivity
  • high thermal conductivity
  • less resistance to heat flow
  • a porous structure
Q.9.Heat flux through several resistance in series in analogous to the current flowing through several
  • resistances in parallel
  • capacitors in series
  • resistances in series
  • none of these
Q.10.The overall resistance for heat transfer through a series of flat resistance, is the ..... of the resistances.
  • average
  • geometric mean
  • product
  • sum
Q.11.Which of the following has the highest thermal conductivity ?
  • Brick
  • Air
  • Water
  • Silver
Q.12.Which area is used in case of heat flow by conduction through a cylinder ?
  • Logarithmic mean area
  • Arithmetic mean area
  • Geometric mean area
  • None of these
Q.13.For heat flow through very thick walled cylinder, use ............ mean radius.
  • arithmetic
  • logarithmic
  • geometric
  • either (a) or (c)
Q.14.What is the logarithmic mean of r1 and r2 ?
  • r1 - r2/ln r1/r2
  • r1 - r2/ln r2/r1
  • r2 - r1/ln r1/r2
  • r1 - r2/ - ln r1/r2
Q.15.What is Nusselt number ?
  • Cp.μ/k
  • hD/k
  • h.Cp/μ
  • Cp.μ/h
Q.16.Prandtl number is given by
  • Cp.μ/a
  • hD/k
  • Cp.μ/k
  • μ/h.Cp
Q.17.Thermal diffusivity is given by
  • k/r.Cp
  • r.Cp/k
  • Cp.μ/a
  • μ/hCp
Q.18.Grashhoff number is given by
  • g D3. β .∆ tr2/μ2
  • g D2β∆tr/μ2
  • g D2β∆tr2μ
  • g D3β∆tr2/μ
Q.19.If h1=inner film co-efficient & h2=outer film co-efficient, then the overall heat transfer co-efficient is
  • always less than h1
  • always between h1 and h2
  • always higher than h2
  • dependent on metal resistance
Q.20.Gratez number is give by
  • mCp/kL
  • kL/mCp
  • mCp/kμ
  • kL/mCp
Q.21.In the equation Q= UA ∆t ; ∆t is
  • geometric mean temperature difference.
  • arithmetic mean temperature difference.
  • logarithmic mean temperature difference.
  • the difference of average bulk temperatures of hot and cold fluids.
Q.22.Peclet number (Pe) is given by
  • Pe = Re.Pr
  • Pe = Re/Pr
  • Pe = Pr/Re
  • Pe = Nu.Re
Q.23.Prandtl number is the reciprocal of
  • Thermal diffusivity/ Momentum diffusivity
  • Thermal diffusivity x Momentum
  • Thermal diffusivity x Mass diffusivity
  • Mass diffusivity x Momentum diffusivity
Q.24.Maximum heat transfer rate is obtained in .......... flow.
  • laminar
  • turbulent
  • creeping
  • transition region
Q.25.Heat flux is the time rate of heat transfer per unit
  • length
  • area
  • volume
  • none of these
Q.26.Nusselt number is the ratio of the
  • temperature gradient of the wall to that across the entire pipe.
  • temperature difference to the temperature gradient at the wall.
  • heat flux at the wall to that across the entire pipe.
  • none of these
Q.27.Fouling factor
  • is a dimensionless quantity.
  • does not provide a safety factor for design.
  • accounts for additional resistances to heat flow.
  • none of these.
Q.28.Viscosity of gases ....... with increase in temperature.
  • increase very rapidly
  • increase slowly
  • decrease slowly
  • remain unaffected
Q.29.Heat transfer co-efficient (h1) for liquids increases with
  • increasing temperature
  • decreasing temperature
  • decreasing Reynolds number
  • none of these
Q.30.At what value of Prandtl number, conduction is negligible in the turbulent core of a fluid flowing through a heated pipe ?
  • 0.5
  • < 0.5
  • > 0.6
  • < 0.1
Q.31.At Pr > 1, conduction in an ordinary fluid flowing through a heated pipe is limited to the
  • buffer zone
  • turbulent core
  • both (a) and (b)
  • viscous sub-layer
Q.32.Conduction occurs in the buffer zone for a fluid flowing through a heated pipe, only when Prandtl number is
  • 0.1
  • > 1
  • < 1
  • 1
Q.33.Natural convection is characterized by
  • Grashhoff number
  • Peclet number
  • Reynolds number
  • Prandtl number
Q.34.Which of the following is unimportant in forced convection ?
  • Reynolds number
  • Prandtl number
  • Grashhoff number
  • none of these
Q.35.In fored convection, the heat transfer depends on
  • Re, Pr
  • Re, Gr
  • mainly Gr
  • Re only
Q.36.The characteristic dimensionless groups for heat transfer to a fluid flowing through a pipe in laminar flow are
  • Re. Gz
  • Nu, Pr
  • Nu, Pr, Re
  • Nu, Gz 
Q.37.At what value of Prandtl number, the hydrodynamic and thermal boundary layers of a fluid flowing over a heated plate will be identical ?
  • 1
  • < 1
  • > 1
  • none of these
Q.38.Reynold's analogy states that
  • St = f/2
  • St = f/4
  • St = 4f
  • St = f1/2
Q.39.For what value of Prandtl number, St = f/2 ?
  • 1.5
  • > 1
  • < 1
Q.40.Which has the lowest Prandtl number ?
  • Liquid metal
  • Aqueous solution
  • Water
  • Lube oil
Q.41.Dietus-Boelter equation used for the determination of heat transfer co-efficient is valid
  • for fluids in laminar flow
  • for fluids in tubulent flow
  • when Grashhoff number is very important
  • for liquid metals
Q.42.For what value of Prandtl number, the Colburn analogy is valid ?
  • 0.06 to 120
  • 0.6 to 120
  • 1 to 103
  • 1 to 50
Q.43.Pick out the correct equation.
  • jH = (St) (Pr)2/3 = f/2
  • jH = (St) (Pr)1/3 = f/2
  • jH = (St)2/3 (Pr) = f/2
  • jH = (St)1/3 (Pr) = f/2
Q.44.Choose the correct equation.
  • Nu = (Re) (Pr) (Gz)
  • Nu = (Re) (Pr) (St)
  • Nu = (Re) (Pr)
  • Nu = (Pr) (St)
Q.45.For a liquid in laminar flow through a very long tube, when the exit fluid temperature approaches the wall temperature, the equation to be used is
  • Nu = 0.023 Re0.8 . Pr0.4
  • Nu = p/2 Gz
  • Nu = 2/p Gz
  • Nu = 2Gz0.5
Q.46.If average heat transfer co-efficient is ha and the local coefficient at the end of the plate is hl then in case of heat transfer to a fluid flowing over a flat plate, heated over its entire length
  • ha = hl
  • ha = 2 hl
  • ha = 0.5 hl
  • ha = 0.75 hl
Q.47.When does the heat generated by fluid friction becomes appreciable compared to the heat transferred between the fluids ?
  • At high fluid velocity
  • At low velocity
  • When fluid flows past a smooth surface
  • None of these
Q.48.The heat transfer co-efficient in film type condensation is ....... that for dropwise condensation.
  • greater than
  • lower than
  • is same as
  • half
Q.49.Prandtl number is the ratio of
  • momentum diffusivity to mass diffusivity
  • momentum diffusivity to thermal diffusivity
  • thermal diffusivity to mass diffusivity
  • thermal diffusivity to momentum diffusivity
Q.50.All analogy equations connecting friction factor and heat transfer co-efficient apply only to
  • wall or skin friction
  • form friction
  • both (a) and (b)
  • turbulent flow
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