Laminar Flow MCQ Quiz in বাংলা - Objective Question with Answer for Laminar Flow - বিনামূল্যে ডাউনলোড করুন [PDF]
Last updated on Mar 10, 2025
Latest Laminar Flow MCQ Objective Questions
Top Laminar Flow MCQ Objective Questions
Laminar Flow Question 1:
The shear stress at a point 5 cm from the pipe axis is 20 Pa. The value of shear stress at the pipe wall, having a diameter of 20 cm will be
Answer (Detailed Solution Below)
Laminar Flow Question 1 Detailed Solution
Explanation:
Shear stress at any distance ‘r’ from the center of the pipe is given by.
\(τ = \frac{{ - r}}{2}\left( {\frac{{\partial p}}{{\partial x}}} \right)\)
At r = R, i.e. at the, pipe wall, shear stress is maximum and is given by
\({τ _{max}} = \frac{{ - R}}{2}\left( {\frac{{\partial p}}{{\partial x}}} \right)\)
Where, R = Radius of the pipe
\(\frac{{\partial p}}{{\partial x}}\) = Pressure gradient over the length of the pipe.
So, from the above, τ ∝ R
Calculation:
Given:
τ = 20 Pa, r = 5 cm, R = 10 cm
\(\frac{τ _{max}}{τ} = \frac Rr\)
\(\frac{τ _{max}}{20} = \frac {10}{5}\)
τmax = 40 Pa
Laminar Flow Question 2:
What can definitely be said about the tube-flow in the diagram below?
Answer (Detailed Solution Below)
Laminar Flow Question 2 Detailed Solution
Explanation:
Laminar Flow: Laminar flow is the flow in which fluid particles flow in layers. Each layer moves smoothly past the adjacent layer with little or no intermixing. There is no intermingling of fluid particles across the cross-section. So laminar flow resembles streamline flow.
Laminar flow through a circular pipe follows parabolic velocity distribution.
From the above diagram, we can see that the velocity distribution in laminar flow is parabolic and the velocity distribution in Turbulent flow is Logarithmic. As in the question figure the velocity distribution parabolic, Hence the given flow is laminar.
Additional Information
For the flow through a circular pipe,
Laminar flow – Reynold’s Number is less than 2000
Turbulent Flow – Reynold’s Number is greater than 4000
Transition Flow – Reynold’s Number is between 2000 to 4000
Laminar Flow Question 3:
For laminar flow through pipes, the Reynolds number should be:
Answer (Detailed Solution Below)
Laminar Flow Question 3 Detailed Solution
Explanation:
Reynolds Number
Reynold number is a dimensionless number that helps to predict flow patterns in different fluid flow situations.
\({\rm{Re}} = \frac{{{\rm{Inertia\;force}}}}{{{\rm{Viscous\;force}}}} = {\rm{\;}}\frac{{{\rm{\rho V}}{{\rm{L}}_{\rm{c}}}}}{{\rm{\mu }}} = \frac{{{\rm{V}}{{\rm{L}}_{\rm{c}}}}}{{\rm{\nu }}}\)
Where,
Re = Reynolds number, ρ = density, V = velocity of flow
μ = dynamic viscosity ν = kinematic viscosity, LC = characteristic linear dimension
For pipe flow:
LC = diameter of pipe = D
Reynold number = \(Re = \frac{{{\rm{\rho VD}}}}{\mu } = \frac{{{\rm{VD}}}}{\nu }\)
- Laminar flow Re ≤ 2000
- Transition flow 2000 ≤ Re ≤ 4000
- Turbulent flow Re ≥ 4000
Additional Information
The Reynolds number value below which flow can be definitely considered to be Laminar flow is called Critical Reynolds number Rc.
The values of the critical Reynolds number are listed below:
- For Pipe flow Rc = 2300
- For Flow between plate Rc = 1000
- For open channel flow Rc = 500
- For flow over plate Rc = 5 × 105
- For flow over sphere Rc = 1
Laminar Flow Question 4:
Match the following non-dimensional numbers the corresponding definitions:
Non-dimensional number |
Definition |
||
P |
Reynolds number |
1 |
(Buoyancy force)/ (Viscous force) |
Q |
Grashof number |
2 |
(Momentum diffusivity)/ (Thermal diffusivity) |
R |
Nusselt number |
3 |
(Inertia force)/ (Viscous force) |
S |
Prandtl number |
4 |
(Convective heat transfer)/ (Conduction heat transfer) |
Answer (Detailed Solution Below)
Laminar Flow Question 4 Detailed Solution
Different dimensionless numbers:
- \(Weber\;Number = \frac{{Inertia\;force}}{{Surface\;tension\;force}}\)
- \(Reynold's\;number = \frac{{Inertia\;force}}{{Viscous\;force}}\)
- \(Mach\;number = \frac{{Inertia\;force}}{{Elastic\;force}}\)
- \(Euler's\;number = \frac{{Inertia\;force}}{{Pressure\;force}}\)
- \(Froude\;number = \frac{{Inertia\;force}}{{Gravity\;force}}\)
- Biot number → Ratio of internal thermal resistance to boundary layer thermal resistance
- Grashof number → Ratio of buoyancy to viscous force
- Prandtl number → Ratio of momentum diffusivity (ν) and thermal diffusivity (α). Pr =ν/α
- Reynolds number → Ratio of inertia force to viscous force
- Nusselt number → Ratio of Convective heat transfer to Conduction heat transfer
- \(Nu = \frac{{h{L_c}}}{k}\)
Laminar Flow Question 5:
Reynold's number is the ratio of
Answer (Detailed Solution Below)
Laminar Flow Question 5 Detailed Solution
Explanation:
Number |
Definition |
Significance |
Reynolds No |
\(Re = \frac{{Inertia\;Force}}{{Viscous\;Force}} \) \(Re =\frac{{\rho VL}}{\mu }\) |
Flow in closed conduit i.e. flow through pipes. |
Froude No |
\(Fr = \sqrt {\frac{{Inertia\;Force}}{{Gravity\;Force}}} \) \(Fr = \frac{V}{{\sqrt {gL} }}\) |
Where a free surface is present and gravity force is predominant. Spillway, Open Channels, waves in the ocean. |
Euler No. |
\({E_u} = \sqrt {\frac{{Inertia\;Force}}{{Pressure\;Force}}} \) \({E_u} =\frac{V}{{\sqrt {\frac{p}{\rho }} }}\) |
In cavitation studies, where pressure force is predominant. |
Mach No. |
\(M = \sqrt {\frac{{Inertia\;Force}}{{Elastic\;Force}}} \) \(M = \frac{V}{C}\) |
Where fluid compressibility is important. Launching of rockets, airplanes and projectile moving at supersonic speed. |
Weber No. |
\({W_e} = \sqrt {\frac{{Inertia\;Force}}{{Surf\;tension\;Force}}} \) \({W_e} =\frac{V}{{\sqrt {\frac{\sigma }{{\rho L}}} }}\) |
In Capillary studies i.e. where Surface tension is predominant. |
Laminar Flow Question 6:
The head loss due to the friction in a pipe of length 9.81 m, diameter 1 m, the velocity of water = 2 m/s and friction factor = 0.06 is:
Answer (Detailed Solution Below)
Laminar Flow Question 6 Detailed Solution
Concept:
Head loss due to friction in a pipe:
\({h_f} = \frac{{f'L{V^2}}}{{2gd}}\)
f’ = Friction factor, L = Length of the pipe, V = average velocity of the fluid in the pipe, g = Acceleration due to gravity, d = Diameter of the pipe
Calculations:
Given:
f’ = 4f = 0.06 (f is friction coefficient), L = 9.81 m, V = 2 m/s, g = 9.81 m/s2, d = 1 m
\({h_f} = \frac{{f'L{V^2}}}{{2gd}}=\frac{0.06~\times~9.81~\times~4}{2~\times~9.81~\times~1}\)
hf = 0.12 mLaminar Flow Question 7:
A sphere of diameter 30 cm is moving with a uniform velocity of 4 m/s. The dynamic viscosity and specific gravity of the liquid are given as 0.8 poises and 0.9 respectively. What is the value of the Reynolds number?
Answer (Detailed Solution Below)
Laminar Flow Question 7 Detailed Solution
Concept:
Reynolds Number Re is defined as the ratio of the Inertia force to viscous force.
Inertia force (Fi) = mass × acceleration
\({{\rm{F}}_{\rm{i}}} = {\rm{ρ }} \times {\rm{volume}} \times \frac{{{\rm{velocity}}}}{{{\rm{time}}}} = {\rm{ρ }} \times {\rm{velocity}} \times \frac{{{\rm{volume}}}}{{{\rm{time}}}} = {\rm{ρ }} \times {\rm{V}} \times {\rm{AV}}\)
Viscous force (Fv) = shear stress × area \(= {\rm{\;}}\tau \times {\rm{A}} = \mu \times \frac{{\rm{V}}}{{\rm{L}}} \times {\rm{A}}\)
Reynolds Number (Re) = \(\frac{{ρ \times {\bf{V}} \times {\rm{L}}}}{\mu }\)
Calculation:
\({{\rm{R}}_{\rm{e}}} = \frac{{{\rm{ρ }} \times {\rm{V}} \times {\rm{d}}}}{{\rm{\mu }}}\)
ρ = 0.9 g/cm3 = 900 kg/m3, V = 4 m/s, d = 30 cm = 0.3 m, μ = 0.8 poise = 0.08 Ns/m2
\({{\rm{R}}_{\rm{e}}} = \frac{{900 \times 4 \times 0.3}}{{0.08}} = 13500\)
Laminar Flow Question 8:
Within a boundary layer for a steady incompressible flow, the Bernoulli equation
Answer (Detailed Solution Below)
Laminar Flow Question 8 Detailed Solution
Explanation:
\(\frac{P}{\rho g} + \frac{{{v^2}}}{{2g}} + Z = Constant\)
Bernoulli’s equation:
- It can be derived from the principle of conservation of energy.
- It states that, in a steady flow, the sum of all forms of energy in a fluid along a streamline is the same at all points on that streamline.
- It represented in head form (the total energy per unit weight).
Following assumption are made in deriving Bernoulli’s equation:
Bernoulli’s equation assumptions:
- The fluid is ideal, i.e. fluid has zero viscosity
- Flow is steady
- Flow is continuous
- Flow is incompressible
- Flow is irrotational
- Flow is along a streamline.
Within a boundary layer for a steady incompressible flow, viscosity is present and the viscous forces dominate over inertia forces.
Thus, the Bernoulli equation does not hold within a boundary layer for a steady incompressible flow.
Laminar Flow Question 9:
In flow through a pipe, the transition from laminar to turbulent flow does not depend on
Answer (Detailed Solution Below)
Laminar Flow Question 9 Detailed Solution
Explanation:
Reynold's number:
- It is a dimensionless number that determines the nature of the flow of liquid through a pipe or flat plate.
- It is defined as the ratio of the inertial force to the viscous force for a flowing fluid.
Reynold's number is written as Re.
\({Re} = \frac{{{\rm{Inertial\;force}}}}{{{\rm{Viscous\;force}}}}\Rightarrow\frac{ρ Vx}{μ}=\frac{Vx}{ν}\)
where ρ = density of fluid, V = velocity of flowing fluid, μ = dynamic viscosity of fluid, ν = kinematic viscosity of fluid and x = characteristic diameter.
where \(x=\frac{4A}{P}\)
and A = area of cross-section and P = perimeter.
Laminar Flow Question 10:
Water is flowing with a velocity of 0.15 m/sec over a plate 1 m long and 0.8 m wide. Calculate the Reynold's number.
[Take viscosity of water µ = 0.001 Ns/m2]
Answer (Detailed Solution Below)
Laminar Flow Question 10 Detailed Solution
Explanation:
Data given,
Velocity of flow, v = 0.15 m/sec
viscosity of water µ = 0.001 Ns/m2
Length of plate, l = 1 m
Reynold's number = ?
Solution:
We know that,
Re = \(ρ.v.l \over µ\) = \(1000 \times 0.15 \times 1 \over 0.001\) = 150,000