UNIT 4: FLUID MECHANICS – II
High-Impact Exam Notes Based on CE-604(A) Past Papers (May 2024 & May 2022)
1. Introduction & Fundamental Properties
Viscosity (High Frequency)
Definition: Measure of a fluid's resistance to flow or deformation due to internal friction.
Newton's Law of Viscosity:
The shear stress (\(\tau\)) in a fluid is directly proportional to the rate of shear strain (velocity gradient).
$$\tau = \mu \frac{du}{dy}$$
where \(\mu\) = dynamic viscosity (Pa·s or N·s/m²).
Importance in Fluid Motion:
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Governs laminar flow characteristics.
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Determines energy loss due to friction in pipes (major head loss).
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Influences boundary layer development and flow separation.
Temperature Effect:
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Liquids: Viscosity ↓ with temperature ↑ (weaker intermolecular forces).
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Gases: Viscosity ↑ with temperature ↑ (increased molecular momentum transfer).
[!TIP]
Exam Focus: May 2024 asked for temperature effects on water (liquid) vs. air (gas). Remember: water viscosity decreases with heating; air viscosity increases.
Surface Tension (Medium Frequency)
Definition: Contractile tendency of a liquid surface due to cohesive forces, measured as force per unit length (N/m).
Jurin’s Law (Capillary Rise/Fall):
$$h = \frac{2\sigma \cos\theta}{\rho g r}$$
where \(h\) = rise/fall height, \(\sigma\) = surface tension, \(\theta\) = contact angle, \(\rho\) = density, \(r\) = capillary radius.
Pressure Difference in Droplets/Bubbles:
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Droplet (single surface): \(\Delta p = \frac{2\sigma}{R}\)
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Soap bubble (two surfaces): \(\Delta p = \frac{4\sigma}{R}\)
[!TIP]
Common Pitfall: In manometer problems (May 2024), capillary rise causes error in pressure reading. Use Jurin’s law to correct if tube diameter is small.
2. Fluid Statics
Pascal’s Law (Medium Frequency)
Statement: Pressure applied to an enclosed fluid is transmitted undiminished to every point in the fluid and the container walls.
Proof (Consider a small fluid element):
Applications:
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Hydraulic press/jack
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Hydraulic brakes
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Hydraulic lifts
Buoyancy & Flotation (Medium Frequency)
Archimedes’ Principle: A body immersed in fluid experiences an upward buoyant force equal to weight of displaced fluid.
Problem-Solving (Multiple Fluids):
For a block floating at interface of two immiscible fluids:
$$\rho_{\text{block}} = \frac{\rho_1 V_1 + \rho_2 V_2}{V_{\text{total}}}$$
where \(V_1, V_2\) = volumes in each fluid.
[!TIP]
May 2024 Question: Wooden block floats differently in water vs. glycerin. Use relative density and volume fractions to solve.
3. Fluid Kinematics
Eulerian vs. Lagrangian Description (Medium Frequency)
| Lagrangian | Eulerian |
|---|---|
| Tracks individual fluid particles | Observes properties at fixed points in space |
| Uses material derivative \(D/Dt\) | Uses partial derivatives \(\partial/\partial t\) |
| Complex for continuum flows | Standard in engineering |
Continuity Equation (High Frequency)
Derivation (3D Cartesian, Steady/Unsteady):
Apply conservation of mass to a control volume:
$$\frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \vec{V}) = 0$$
For incompressible flow (\(\rho = \text{constant}\)):
$$\nabla \cdot \vec{V} = 0 \quad \text{or} \quad \frac{\partial u}{\partial x} + \frac{\partial v}{\partial y} + \frac{\partial w}{\partial z} = 0$$
Finding Missing Velocity Component (May 2022):
Given \(u(x,y,z)\) and \(v(x,y,z)\), integrate \(\partial w/\partial z = -(\partial u/\partial x + \partial v/\partial y)\) to find \(w(z)\).
Stream Function & Velocity Potential (High Frequency)
Stream Function (\(\psi\)):
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Defined for 2D incompressible flow: \(u = \frac{\partial \psi}{\partial y},\; v = -\frac{\partial \psi}{\partial x}\)
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Automatically satisfies continuity.
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Lines of constant \(\psi\) = streamlines.
Velocity Potential (\(\phi\)):
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Defined for irrotational flow: \(u = \frac{\partial \phi}{\partial x},\; v = \frac{\partial \phi}{\partial y}\)
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Lines of constant \(\phi\) = equipotential lines.
Orthogonal Trajectories:
Streamlines and equipotentials intersect at 90° because:
$$\nabla \phi \cdot \nabla \psi = u \cdot u + v \cdot (-v) = u^2 - v^2 \quad \text{? Wait, correction:}$$
Actually:
$$\nabla \phi = (u, v), \quad \nabla \psi = (v, -u) \quad \Rightarrow \quad \nabla \phi \cdot \nabla \psi = uv - vu = 0$$
[!TIP]
May 2024: Given \(\phi = x(2y-1)\), find velocity at P(4,5) and \(\psi\) at P.
Solution: \(u = \partial\phi/\partial x = 2y-1 = 9\), \(v = \partial\phi/\partial y = 2x = 8\). Then \(\psi\) from \(d\psi = u\,dy - v\,dx\) → integrate.
Flow Nets (Medium Frequency)
Construction: Orthogonal grid of streamlines and equipotentials.
Applications:
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Groundwater flow through soils
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Seepage under dams
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Laplace equation solutions (\(\nabla^2 \phi = 0, \nabla^2 \psi = 0\))
Properties:
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Each "square" represents equal flow rate and equal head drop.
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Density of lines indicates velocity magnitude.
4. Fluid Dynamics
Euler’s Equation of Motion (High Frequency)
Derivation along a Streamline:
Consider a fluid element of length \(ds\) along streamline. Forces: pressure, weight, inertia.
$$-dp - \rho g\,dz = \rho \frac{DV}{Dt} ds$$
For steady flow: \(\frac{DV}{Dt} = V\frac{dV}{ds}\)
$$\boxed{-dp = \rho V\,dV + \rho g\,dz}$$
Bernoulli’s Theorem (High Frequency)
Derivation: Integrate Euler’s equation for steady, incompressible, inviscid, along a streamline:
$$\boxed{\frac{p}{\rho} + \frac{V^2}{2} + gz = \text{constant}}$$
or
$$\boxed{p + \frac{1}{2}\rho V^2 + \rho gz = \text{constant}}$$
Assumptions:
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Steady flow
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Incompressible fluid
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Inviscid (zero viscosity)
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Along a streamline
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No shaft work/heat transfer
Limitations:
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Not valid in viscous boundary layers, wakes, or highly turbulent regions.
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Does not account for friction losses (use with correction factors).
Applications:
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Venturi meter, orifice meter
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Pitot tube (velocity measurement)
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Flow through pipes with varying area
Total Energy Line (TEL) & Hydraulic Gradient Line (HGL) (High Frequency)
| TEL (Energy Grade Line) | HGL (Hydraulic Grade Line) |
|---|---|
| Represents total head: \(H = \frac{p}{\rho g} + \frac{V^2}{2g} + z\) | Represents piezometric head: \(h = \frac{p}{\rho g} + z\) |
| Always above HGL by velocity head \(\frac{V^2}{2g}\) | Lies below TEL |
| Slope indicates head loss (friction + minor) | Slope indicates pressure head variation |
Representation in Piping Systems:
[!TIP]
Exam Distinction: TEL includes kinetic energy; HGL does not. In a horizontal pipe with constant diameter, HGL is parallel to TEL but lower by constant velocity head.
5. Pipe Flow & Boundary Layer Theory
Laminar Flow in Circular Pipes (High Frequency)
Velocity Distribution (Parabolic):
$$u(r) = u_{\text{max}} \left(1 - \frac{r^2}{R^2}\right)$$
where \(u_{\text{max}} = 2V_{\text{avg}}\).
Shear Stress:
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At wall (\(r=R\)): \(\tau_w = \mu \left.\frac{du}{dr}\right|_{r=R} = \frac{\Delta p \cdot R}{2L}\)
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At any radius \(r\): \(\tau(r) = \tau_w \cdot \frac{r}{R}\)
Volumetric Flow Rate (Hagen-Poiseuille):
$$Q = \frac{\pi R^4 \Delta p}{8\mu L}$$
Reynolds Experiment (Medium Frequency)
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Introduced dimensionless Reynolds number: \(Re = \frac{\rho V D}{\mu}\)
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Critical \(Re\):
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For pipe flow: \(Re_{\text{crit}} \approx 2000-2300\) (transition range)
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Laminar: \(Re < 2000\)
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Turbulent: \(Re > 4000\)
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Turbulence (Medium Frequency)
Characteristics:
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Irregular, chaotic fluctuations in velocity/pressure.
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Enhanced momentum/heat/mass transfer.
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Increased energy dissipation (higher friction factor).
Effects:
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Velocity profile flatter (more uniform).
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Pressure drop increases (Darcy-Weisbach \(f\) higher).
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Noise and vibration.
Boundary Layer Theory (High Frequency)
Development on Flat Plate:
Key Thicknesses:
- Displacement thickness (\(\delta^*\)):
$$\delta^* = \int_0^\delta \left(1 - \frac{u}{U}\right) dy$$
Represents outward shift of streamline due to slowing.
- Momentum thickness (\(\theta\)):
$$\theta = \int_0^\delta \frac{u}{U}\left(1 - \frac{u}{U}\right) dy$$
Represents momentum deficit.
-
Boundary layer thickness (\(\delta\)):
\(u(\delta) \approx 0.99U\) (arbitrary but standard).
Laminar vs. Turbulent BL:
| Laminar BL | Turbulent BL |
|---|---|
| Smooth, orderly | Chaotic, mixing |
| \(\delta \propto x^{1/2}\) | \(\delta \propto x^{4/5}\) |
| Thinner | Thicker |
| Lower skin friction drag initially | Higher skin friction but delays separation |
Shear Stress Distribution:
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Laminar: \(\tau = \mu \frac{du}{dy}\), max at wall.
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Turbulent: \(\tau = \mu \frac{du}{dy} - \rho \overline{u'v'}\), includes Reynolds stress.
[!TIP]
May 2024 Question: Calculate friction drag, boundary layer thickness, shear stress at trailing edge for a plate in oil flow. Use Blasius solution for laminar BL: \(\delta \approx 5.0 x / \sqrt{Re_x}\), \(C_f = 0.664 / \sqrt{Re_x}\).
6. Flow Measurement & Instrumentation
Manometers (High Frequency)
Principle: Pressure difference balanced by liquid column height difference.
$$\Delta p = (\rho_m - \rho_f) g h$$
for inclined/differential manometers.
Simple vs. Differential Manometer:
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Simple: One limb open to atmosphere → measures gauge pressure.
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Differential: Both limbs connected to pressure points → measures \(\Delta p\).
Capillary Correction (May 2024):
Error in small tubes due to meniscus curvature.
Given gauge pressure \(p\), tube radius \(r\), surface tension \(\sigma\), contact angle \(\theta\):
Capillary rise \(h_c = \frac{2\sigma \cos\theta}{\rho_m g r}\)
True pressure: \(p_{\text{true}} = p_{\text{measured}} \pm \rho_m g h_c\) (sign depends on meniscus shape).
[!TIP]
May 2024 Problem: Find smallest manometer tube diameter so capillary error < 5% for \(p = 100\,\text{N/m}^2\). Use water as manometric liquid (\(\sigma \approx 0.0728\,\text{N/m}\), \(\theta \approx 0^\circ\)).
Solution: Error \(\% = \frac{\rho_m g h_c}{p} \times 100 < 5\) → solve for \(r\).
Pitot Tube (Medium Frequency)
Working: Stagnation pressure measured at nose; static pressure on side taps.
Velocity Calculation:
$$V = \sqrt{\frac{2(p_0 - p_s)}{\rho}}$$
where \(p_0\) = stagnation pressure, \(p_s\) = static pressure.
Applications:
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Aircraft airspeed measurement
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Flow velocity in pipes/channels
7. Applications of Fluid Mechanics
Reciprocating Pump (Low Frequency)
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Positive displacement pump.
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Piston/plunger reciprocates in cylinder.
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Suction and delivery valves control flow direction.
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Pulsating flow; requires air vessel for smoothing.
Reaction Turbine (Low Frequency)
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Pressure energy → kinetic energy → mechanical work.
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Examples: Francis, Kaplan turbines.
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Water flows over fixed blades ( stator ) then rotating blades ( rotor ), generating torque.
Biofluid Mechanics (Low Frequency)
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Blood flow in veins: Low Reynolds number, often laminar; influenced by gravity, valves.
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Heart pumping: Pulsatile flow; compliance of arteries dampens pulses.
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Reynolds number in aorta: \(Re \sim 2000\), transitional; laminar in capillaries.
8. Advanced Concepts
Fluid Deformation under Sustained Shear Stress
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Newtonian fluids: Constant viscosity, linear \(\tau\) vs. \(\dot{\gamma}\).
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Non-Newtonian:
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Dilatant: \(\mu \uparrow\) with \(\dot{\gamma} \uparrow\) (e.g., cornstarch-water)
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Pseudoplastic: \(\mu \downarrow\) with \(\dot{\gamma} \uparrow\) (e.g., paint, blood)
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Bingham plastic: Yield stress required (e.g., toothpaste).
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Key Formulas Boxed
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Newton’s Law: \(\boxed{\tau = \mu \frac{du}{dy}}\)
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Continuity (incompressible): \(\boxed{\frac{\partial u}{\partial x} + \frac{\partial v}{\partial y} + \frac{\partial w}{\partial z} = 0}\)
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Euler’s Equation: \(\boxed{-dp = \rho V dV + \rho g dz}\)
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Bernoulli’s Theorem: \(\boxed{\frac{p}{\rho} + \frac{V^2}{2} + gz = \text{constant}}\)
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Laminar Pipe Flow (Hagen-Poiseuille): \(\boxed{Q = \frac{\pi R^4 \Delta p}{8\mu L}}\)
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Boundary Layer Shear Stress (laminar): \(\boxed{\tau_w = \mu \left.\frac{du}{dy}\right|_{y=0} = 0.332 \rho U^2 / \sqrt{Re_x}}\)
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Manometer \(\Delta p\): \(\boxed{\Delta p = (\rho_m - \rho_f) g h}\)
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Pitot Tube Velocity: \(\boxed{V = \sqrt{\frac{2(p_0 - p_s)}{\rho}}}\)
Diagram References for Study
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Laminar velocity profile in pipe: Search: "parabolic velocity profile laminar flow pipe"
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Boundary layer on flat plate: Search: "laminar turbulent boundary layer thickness flat plate"
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Flow net through earth dam: Search: "flow net seepage under dam"
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Pitot-static tube: Search: "Pitot tube stagnation static pressure"
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TEL & HGL in piping system: Search: "energy grade line hydraulic grade line pipe"
Final Exam Strategy:
- May 2024 & 2022 heavily tested viscosity, Bernoulli, continuity, boundary layer, manometers.
- Always state assumptions before applying Bernoulli.
- For continuity problems, write the 3D equation first, then simplify.
- In boundary layer questions, recall \(\delta \propto x/\sqrt{Re_x}\) for laminar.
- For capillary correction in manometers, compute \(h_c\) and adjust pressure.
- Derive Euler → Bernoulli stepwise; it’s a sure 7-mark question.