ME-404 · FLUID MECHANICS/Unsolved PYQ Paper
ME-404 Fluid Mechanics - Dec 2024 Question Paper
Under each question, How to answer lists the points an answer should cover, outlined by CampusPrep from the syllabus. Check the details against your textbook.
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7 MarksaDetermine the Bulk modulus of elasticity of a liquid, if the pressure of the liquid is increased from $70 N/cm^2$ to $130 N/cm^2$. The volume of the liquid decreases by $0.15\%$.
How to answer
- Define bulk modulus $K = -V dp/dV = dp/(-dV/V)$
- Convert pressure rise $dp = 130-70 = 60\, N/cm^2$
- Use volumetric strain $dV/V = -0.15\% = -0.0015$
- Compute $K$ and express in $N/cm^2$ / $MN/m^2$
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7 MarksbDefine the terms Dynamic viscosity and Kinematic viscosity. State their units of measurement.
How to answer
- Define dynamic viscosity $\mu$ from Newton's law of viscosity
- Define kinematic viscosity $\nu = \mu/\rho$
- State SI units: $Pa\cdot s$ and $m^2/s$
- Mention measurement units poise, stokes
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7 MarksaDefine stream function and velocity potential function. Prove that stream lines and equipotential lines meet each other orthogonally.
How to answer
- Define stream function $\psi$ and velocity potential $\phi$ with $u,v$ relations
- Write $d\psi=0$ for streamline and $d\phi=0$ for equipotential
- Derive slopes $dy/dx$ for both lines
- Show product of slopes $=-1$, hence orthogonal
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7 MarksbA stream functions in two dimensional flow $\psi = 2xy$. Determine the corresponding velocity potential $\Phi$.
How to answer
- Obtain $u,v$ from $\psi = 2xy$ using $u=\partial\psi/\partial y$, $v=-\partial\psi/\partial x$
- Use Cauchy-Riemann $u=\partial\Phi/\partial x$, $v=\partial\Phi/\partial y$
- Integrate to get $\Phi(x,y)$
- Check irrotational / Laplace equation
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7 MarksaA man weighing 90 kgf descends to the ground from an aeroplane with the help of a parachute against the resistance of air the velocity with which the parachute, which the hemispherical in shape comes down is 20 m/s. Find the diameter of parachute. Assume CD= 0.5 and density of air $1.25 kg/m^3$.
How to answer
- Equate weight $W=90\,kgf$ to drag $F_D = C_D A \rho V^2/2$
- Take projected area of hemispherical parachute $A=\pi D^2/4$
- Substitute $V=20\,m/s$, $C_D=0.5$, $\rho=1.25\,kg/m^3$
- Solve for $D$
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7 MarksbState and prove Bernoulli's theorem. Mention the assumptions made. How is it modified while applying in real problem?
How to answer
- State Bernoulli's theorem $p/\rho g + V^2/2g + z =$ constant
- List assumptions: steady, incompressible, inviscid, along streamline
- Derive from Euler's equation by integration
- Add loss term $h_L$ and coefficients for real fluid application
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7 MarksaWhat are the minor losses and major losses in a pipe flow? Derive the chazy's formula for the loss of head due to friction.
How to answer
- Define major loss due to friction and list minor losses
- Consider force balance on pipe element
- Relate wall shear to pressure drop
- Obtain Chezy's $V = C\sqrt{mi}$ and head loss form
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7 MarksbA laminar flow is taking place in a pipe of diameter 200 mm. The maximum velocity is 1.5m/s. Find the mean velocity and the radius at which this occurs. Also calculate the velocity at 4 cm from the wall of pipe. Find :
- i)Mean velocity, ū
- ii)A Radius at which ū occurs
- iii)Velocity at 4 cm from the wall
How to answer
- Use parabolic profile $u = U_{max}[1-(r/R)^2]$ so $\bar u = U_{max}/2$
- Find radius where $u=\bar u$: $r = R/\sqrt{2}$
- Compute velocity at $4\,cm$ from wall i.e. $r = R-0.04$
- Substitute $D=200\,mm$, $U_{max}=1.5\,m/s$
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7 MarksaExplain separation of boundary layer. What is the effect of pressure gradient on boundary layer separation?
How to answer
- Define boundary layer separation and separation point
- Explain adverse pressure gradient $dp/dx>0$ effect
- Describe backflow and wake formation
- Mention control methods
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7 MarksbDerive expression for the velocity distribution for viscous flow through a circular pipe.
How to answer
- Consider steady laminar flow in circular pipe, Hagen-Poiseuille assumptions
- Apply Navier-Stokes / force balance on fluid element
- Integrate with no-slip at wall and symmetry at centre
- Obtain parabolic $u(r)$ and mean velocity
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14 MarksFind the Momentum thickness, and Energy thickness for the velocity distribution in the boundary layer is given by: $$\frac{u}{U} = 2\left\{\frac{y}{\delta}\right\} - \left\{\frac{y}{\delta}\right\}^2$$
How to answer
- Recall $\theta = \int_0^\delta (u/U)(1-u/U)dy$, $\delta^*_e = \int_0^\delta (u/U)(1-(u/U)^2)dy$
- Substitute $u/U = 2\eta-\eta^2$ with $\eta=y/\delta$
- Integrate term-wise from 0 to 1
- Express results as fractions of $\delta$
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7 MarksaExplain the following terms:
- i)Magnus effect
- ii)Stagnation point
- iii)Airfoil
How to answer
- Define Magnus effect with rotating cylinder lift
- Define stagnation point where velocity is zero
- Define airfoil and its lift generation
- Give examples / diagrams
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7 MarksbFind the density of a metallic body which floats at the interface of mercury of specific gravity 13.6 and water such that 40% of its volume is submerged in mercury and 60% in water.
How to answer
- Equate weight of body to buoyancy from mercury + water
- Write $\rho V = 0.4V\rho_{Hg}+0.6V\rho_{w}$
- Use $\rho_{Hg}=13.6\times1000\,kg/m^3$
- Solve for $\rho$
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7 MarksaWrite about Venturimeter. Derive the expression for rate of flow of fluid through Venturimeter.
How to answer
- Describe Venturimeter parts: convergent, throat, divergent + manometer
- Apply Bernoulli and continuity between inlet and throat
- Include discharge coefficient
- Obtain $Q = C_d A_1A_2\sqrt{2gh}/\sqrt{A_1^2-A_2^2}$
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7 MarksbA 30 cm diameter pipe, conveying water, branches into two pipes of diameters 20 cm and 15 cm respectively. The average velocity in the 30 cm diameter pipe is 2.5 m/s, find the discharge in this pipe. Also determine the velocity in 15 cm pipe if the average velocity in 20 cm diameter pipe in 2 m/s.
How to answer
- Compute $Q = A_{30}V_{30}$ with $D=30\,cm$, $V=2.5\,m/s$
- Apply continuity $Q = Q_{20}+Q_{15}$
- Compute $Q_{20}=A_{20}\times2\,m/s$
- Solve for $V_{15} = (Q-Q_{20})/A_{15}$
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