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Download ARPIT 2020 Convective Heat Transfer Fundamentals And Applications Creation Question Paper

Download Annual Refresher Programme in Teaching (ARPIT) 2020 Convective Heat Transfer Fundamentals And Applications Creation Previous Question Paper || Annual Refresher Programme in Teaching (ARPIT) Last 10 Years Question Paper

This post was last modified on 19 January 2021

ARPIT Last 10 Years 2011-2021 Previous Question Papers


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Question Paper Name : Convective Heat Transfer Fundamentals and Applications 2020 Shift 1

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Subject Name : Convective Heat Transfer Fundamentals and Applications

Creation Date : 2020-09-15 13:26:34

Duration : 180

Total Marks : 75

Display Marks: Yes

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Share Answer Key With Delivery Engine : Yes

Actual Answer Key : Yes

Convective Heat Transfer Fundamentals and Applications

Group Number : 1

Group Id : 8995146

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Group Maximum Duration : 0

Group Minimum Duration : 120

Show Attended Group? : No

Edit Attended Group? : No

Break time : 0

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Group Marks : 75

Is this Group for Examiner? : No

Convective Heat Transfer Fundamentals and Applications

Section Id : 8995146

Section Number : 1

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Section type : Online

Mandatory or Optional : Mandatory

Number of Questions : 75

Number of Questions to be attempted : 75

Section Marks : 75

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Display Number Panel : Yes

Group All Questions: Yes

Mark As Answered Required? : Yes

Sub-Section Number : 1

Sub-Section Id : 8995146

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Question Shuffling Allowed : Yes

Question Number : 1 Question Id : 899514441 Question Type : MCQ Option Shuffling : No Display Question Number: Yes

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Correct Marks : 1 Wrong Marks : 0

General motion of a fluid particle consists of the following

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(A) Translation only

(B) Linear deformation only

(C) Rotation only

(D) Translation, linear deformation, rotation and angular deformation

Question Number : 2 Question Id : 899514442 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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? ? Cross derivatives like (u is the velocity in the x-direction and v is ?'? the y-direction) cause the fluid element to

(A) Undergo linear deformation

(B) Undergo Translation

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(C) Rotate and undergo angular deformation

(D) Linear deformation and translation

Question Number : 3 Question Id : 899514443 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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Correct Marks : 1 Wrong Marks : 0

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For an incompressible steady flow, the continuity equation is given by

? ? ? (A) [+u+ve+wa+pa++) = 0

? ? ? W

? ? ? (B)+u+vol+w] = 0

?

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W = 0

? ? ? (C) [u+vol+w]

? ?

? ? dw (D) + + = 0

?

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?

dz

Question Number : 4 Question Id : 899514444 Question Type : MCQ Option Shuffling : No Display Question Number: Yes

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Correct Marks : 1 Wrong Marks : 0

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Body forces acting on the fluid element are caused by

(A) Normal stresses, shear stresses and pressure acting on the fluid element

(B) Gravity forces, normal stresses, shear stresses acting on the fluid

(C) Shear stresses, Coriolis force, centrifugal force acting on the fluid

(D) Gravity forces, Coriolis forces and centrifugal forces acting on

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Question Number : 5 Question Id : 899514445 Question Type : MCQ Option Shuffling : No Display Question Number: Yes

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Correct Marks : 1 Wrong Marks : 0

Non-dimensionalisation of the energy equation results in the following numbers

(A) Reynolds number, Prandtl number and Eckert number

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(B) Reynolds number and Prandtl number

(C) Reynolds number and Eckert number

(D) Prandtl number and Eckert number

Question Number : 6 Question Id : 899514446 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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For high speed supersonic flows (high Mach number flows), the following dimensional numbers are important

(A) Reynolds number, Prandtl number and Eckert number

(B) Reynolds number and Prandtl number

(C) Reynolds number and Eckert number

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(D) Prandtl number and Eckert number

Question Number : 7 Question Id : 899514447 Question Type : MCQ Option Shuffling : No Display Question Number: Yes

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Correct Marks : 1 Wrong Marks : 0

In the buffer layer (overlap layer) of the three layer structure of the body following statement is true

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(A) Laminar shear stress (Tlam) >>> Turbulent shear stress (Tturb)

(B) Laminar shear stress Tlam ~ Turbulent shear stress (Tturb)

(C) Laminar shear stress Tlam<<< Turbulent shear stress (Tturb )

(D) None of the above

Question Number : 8 Question Id : 899514448 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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1

= 2.0log(Revf) – 0.8 is derived on the basis of

vf

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(A) Universal velocity distribution and drawing constants from experiment

(B) Purely experimental results (empirical approach)

(C) Purely on the basis of universal velocity distribution

(D) None of the above

Question Number : 9 Question Id : 899514449 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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1

e

= 2.0log() is applicable for

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vf

3.7

(A) Fully developed Laminar flow and hydraulically smooth pipe

(B) Fully developed Laminar flow and hydraulically rough pipe

(C) Fully developed Turbulent flow and hydraulically smooth pipe

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(D) Fully developed Turbulent flow and hydraulically rough pipe

Question Number : 10 Question Id : 899514450 Question Type : MCQ Option Shuffling : No Display Question Number: Yes

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A pipe is said to be hydraulically rough pipe, if the following condition is satisfied

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(A) Roughness elements are geometrically small enough that they can be in viscous sublayer

(B) It is the geometrical roughness which matters, but not the viscous thickness

(C) Roughness elements are geometrically large enough, they break the viscous sublayer

(D) None of the above

Question Number : 11 Question Id : 899514451 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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In a hydraulically rough pipe, the friction factor in a fully developed turbulent function of

(A) Reynolds number and geometrical roughness

(B) Reynolds number only

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(C) Geometrical roughness only

(D) Independent of both Reynolds number and geometrical roughness

Question Number : 12 Question Id : 899514452 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

Line Question Option : No Option Orientation : Vertical

Correct Marks : 1 Wrong Marks : 0

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The fluctuating component of the velocity in a turbulent flow is measured by

(A) Pitot tube and manometer

(B) Hot wire anemometer

(C) Pitot tube alone

(D) None of the above

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Question Number : 13 Question Id : 899514453 Question Type : MCQ Option Shuffling: No Display Question Number : Yes

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Correct Marks : 1 Wrong Marks : 0

In external and internal flows, the solution of the mass and momentum equation velocity distribution and pressure. This information is used to calculate the

(A) Hydrodynamic boundary layer thickness and skin friction coefficient

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(B) Hydrodynamic boundary layer thickness alone

(C) Skin friction coefficient alone

(D) None of the above

Question Number : 14 Question Id : 899514454 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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Correct Marks : 1 Wrong Marks : 0

Consider flow over a flat plate with a Reynolds number of 10000 maintained at constant wall temperature, the essential condition for satisfying analogy is as follows

(A) Prandtl number is to be lower than unity

(B) Prandtl number is to be greater than unity

(C) Prandtl number is required to be unity

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(D) None of the above

Question Number : 15 Question Id : 899514455 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

Line Question Option : No Option Orientation : Vertical

Correct Marks : 1 Wrong Marks : 0

Consider a vertical hot body immersed in a quiescent cold fluid in which steady and natural convection is laminar. Non-dimensionalisation of the equation results in the following non-dimensional numbers

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(A) Grashoff number and Reynolds number

(B) Grashoff number, Reynolds number and Prandtl number

(C) Reynolds number and Prandtl number

(D) Reynolds number, Grashoff number and Eckert number

Question Number : 16 Question Id : 899514456 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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Consider natural convection for either internal flow or external flow following statement is correct

(A) Momentum equation and energy equation are uncoupled

(B) Momentum equation and energy equation are coupled

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(C) Velocity profile can be obtained from momentum equation and temperature profile can be obtained from energy equation

(D) Velocity profile and temperature profile can be obtained by solving equation

Question Number : 17 Question Id : 899514457 Question Type : MCQ Option Shuffling: No Display Question Number: Yes

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Correct Marks : 1 Wrong Marks : 0

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Consider natural convection for vertical hot plates, the critical Grashoff number

(A) Around 2 × 105

(B) Around 2300

(C) Around 100

(D) Around 109

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Question Number : 18 Question Id : 899514458 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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For high Prandtl number fluids, in natural convection for external surface thermal boundary layer, it is the balance of the following forces

(A) Inertia force and friction force

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(B) Inertia force and Buoyancy force

(C) Friction force and buoyancy force

(D) Inertia forces, Friction force and Buoyancy force

Question Number : 19 Question Id : 899514459 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

Line Question Option : No Option Orientation : Vertical

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Correct Marks : 1 Wrong Marks : 0

Consider natural convection around a vertical hot plate maintained at constant temperature surrounded by a low Prandtl number fluid, the scale of the thermal layer is

(A) HRAH

1

1

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(B) HRa

1

1

(C) HRa1*Pr¯¯

1

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1

(D)HRa1²Pr¯¯

where H is the height of the vertical plate and RaH is the Rayleigh number the height of the vertical plate

Question Number : 20 Question Id : 899514460 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

Line Question Option : No Option Orientation : Vertical

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Consider natural convection around a vertical hot plate maintained temperature surrounded by a high Prandtl number fluid, the scale of the is

(A) Ra

(B) Ra

1

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H

1

2

?

(C) RaPr

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1

1-4

(D) RaPr

1-2

where H is the height of the vertical plate and RaH is the Rayleigh number the height of the vertical plate

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Question Number : 21 Question Id : 899514461 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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Correct Marks : 1 Wrong Marks : 0

Which of the following statement is TRUE?

(A) a radiation analysis should normally accompany a natural convection unless the emissivity of the surface is low

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(B) a radiation analysis should normally accompany a natural convection unless the emissivity of the surface is high

(C) radiation analysis may be neglected during natural convection irrespective of the emissivity of the surface

(D) None of the above

Question Number : 22 Question Id : 899514462 Question Type : MCQ Option Shuffling: No Display Question Number: Yes

Line Question Option : No Option Orientation : Vertical

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Correct Marks : 1 Wrong Marks : 0

The assumptions involved in the Nusselt condensation are as follows

(A) Laminar flow and constant properties are assumed for the liquid

(B) Gas is assumed to be pure vapour and at a uniform temperature equal

(C) Shear stress at the liquid-vapour interface is assumed to be negligible

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(D) All of the above

Question Number : 23 Question Id : 899514463 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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Correct Marks : 1 Wrong Marks : 0

In the Nusselt condensation, it is the balance of the following forces

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(A) Inertia force, sinking effect (force) and friction force

(B) Inertia force and friction force

(C) Friction force and sinking effect (force)

(D) Inertia force and sinking effect (force)

Question Number : 24 Question Id : 899514464 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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For a flow over a flat plate with no suction/blowing, constant u8and case of Pr > 1, the flow field is split into the following three regions:

Region I: 0 = y = 8t

Region II: dt = y = d

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Region III: y = d

Which of the following is TRUE for Region III?

(A) u(x, y) < u8 and T(x,y) < T8

(B) u(x, y) = u and T(x,y) = T8

(C) u(x, y) < u8 and T(x,y) > T8

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(D) u(x, y) = u and T(x,y) > T8

Question Number : 25 Question Id : 899514465 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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For a flow over a flat plate with no suction/blowing, constant u8and case ofPr ~ 1, what can you say about the flow field?

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(A) 0 = y = (d or d1) for u = u8 and T > T8

(B) 0 = y = (d ? d1) for u < u8 and T > To8

(C) 0 = y = (d or dt) for u < u8 and T = T8

(D) 0 = y = (8 or 8t) for u > u and T = T8

Question Number : 26 Question Id : 899514466 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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For a flow over a flat plate with no suction or blowing, constant u

u

y

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profile is - = a + by + cn² where, (? = ); the values of a, b, c are

U8

d(x)

(A) 1, -1, -2

(B) 0, 1, -2

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(C) 0, -1, 2

(D) 0, 2, -1

Question Number : 27 Question Id : 899514467 Question Type : MCQ Option Shuffling: No Display Question Number: Yes

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Correct Marks : 1 Wrong Marks : 0

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For a flow over a flat plate with no suction or blowing, constant u

u

y

profile is = 2? – ?² where, (? = ); displacement thickness is:

Uoo

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d(x)

28

(A)

3

(B)

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d

3

2

(C)

3

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1

(D)

3

Question Number : 28 Question Id : 899514468 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

Line Question Option : No Option Orientation : Vertical

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For a flow over a flat plate with no suction or blowing, constant u8, if the

u

y

is- = 2? – ?² where, (? = ); the momentum thickness 82 is:

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U8

d(x)

2

(A)

3

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28

3

(B)

28

15

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(C)

2

15

(D)

Question Number : 29 Question Id : 899514469 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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u

y

Tw-T(x,y)

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For the velocity profile = 2? – ?² and = ?t

Uoo

Tw-Too

?); for Pr = 1, the enthalpy thickness is equal to:

d(x)

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dt(x)

88

(A)

15

28

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(B)

15

(C) 0

(D) dt

Question Number : 30 Question Id : 899514470 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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For laminar flow through a circular pipe of radius R, the velocity distribution

r

u(x) = c [1-2] (where, c is a constant), the bulk mean velocity is:

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R

C

(A)

3

C

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(B)

2

(C) c

2c

(D)

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3

Question Number : 31 Question Id : 899514471 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

Line Question Option : No Option Orientation : Vertical

Correct Marks : 1 Wrong Marks : 0

For laminar flow through a circular pipe of radius R, the velocity distributions are given by u(r) = C and T(r) = D[1-2] respectively and D are constants), the bulk mean temperature is:

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r

R

4D

(A)

5

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2D

(B)

3

D

(C)

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2

(D) D

Question Number : 32 Question Id : 899514472 Question Type : MCQ Option Shuffling: No Display Question Number : Yes

Line Question Option : No Option Orientation : Vertical

Correct Marks : 1 Wrong Marks : 0

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For flow over a flat plate, the flow velocity is decreased by a factor of other variables constant in case of a laminar flow, the boundary

(A) Increases by a factor of 2

(B) Decreases by a factor of 2

(C) Increases by a factor of 4

(D) Decreases by a factor of 4

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Question Number : 33 Question Id : 899514473 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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For a flow over a flat plate, the free stream velocity is increased by a factor all other variables constant. If fluid has Pr << 1, which of the following is

(A) 8 and 8t both decrease

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(B) 8 and 8t both increase

(C) & decreases and dremains unchanged

(D) 8 remains unchanged and dedecreases

Question Number : 34 Question Id : 899514474 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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Correct Marks : 1 Wrong Marks : 0

If blowing velocity is increased, boundary layer thickness

(A) remains unchanged

(B) increases

(C) decreases

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(D) changes randomly

Question Number : 35 Question Id : 899514475 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

Line Question Option : No Option Orientation : Vertical

Correct Marks : 1 Wrong Marks : 0

For the case of thin thermal boundary layer (de « d) over a flat plate number is given by Nux~Re/2Pr¹³/3. For a fixed location in the flow- number is increased from 1600 to 2500, the ratio of the old to the new Nu that location would be

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1

1

(A) 16:25

(B) 25:16

(C) 5:4

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(D)4:5

Question Number : 36 Question Id : 899514476 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

Line Question Option : No Option Orientation : Vertical

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For a circular pipe whose diameter decreases linearly along the flow direction mass flow rate and constant properties, the Reynolds Number of flow flow direction.

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(A) Remains constant

(B) Decreases

(C) Increases

(D) Depends on fluid

Question Number : 37 Question Id : 899514477 Question Type : MCQ Option Shuffling : No Display Question Number : Yes

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For a circular pipe whose diameter decreases linearly along the flow direction mass flow rate and constant properties, the bulk mean velocity a direction.

(A) Remains constant

(B) Decreases

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(C) Increases

(D) Depends on Prandtl number

Question Number : 38 Question Id : 899514478 Question Type : MCQ Option Shuffling : No Display Question Number: Yes

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Correct Marks : 1 Wrong Marks : 0

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Arrange the phenomenon according decreasing values of heat transfer associated with them.

P. Natural convection in water

This download link is referred from the post: ARPIT Last 10 Years 2011-2021 Previous Question Papers

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