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22-Mec-A6 Fluid Machinery · December 2019

Question 4 of 6: Combined Couette–Poiseuille Flow between Parallel Plates

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. National Exams — December 2019, 16-Mec-A6 Advanced Fluid Mechanics. Open book, 3 hours. Six questions of equal value (20 marks); any five constitute a complete paper. All six are solved here as a study resource.

Reference texts. J.D. Anderson, Modern Compressible Flow, 3rd ed. (Q1); Kundu, Cohen & Dowling, Fluid Mechanics, 6th ed. and F.M. White, Fluid Mechanics, 8th ed. (Q2, Q5); F.M. White, Fluid Mechanics, 8th ed. (Q3); F.M. White, Viscous Fluid Flow, 3rd ed. (Q4, Q6); Schlichting & Gersten, Boundary-Layer Theory, 8th ed. (Q6); Fox & McDonald, Introduction to Fluid Mechanics, 10th ed. (general).

Question 4: Combined Couette–Poiseuille Flow between Parallel Plates (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. Steady, incompressible, two-dimensional flow of a Newtonian fluid between horizontal parallel plates a distance $2b$ apart; the top plate moves at $U$ and a constant $dp/dx$ acts along $x$.

Find. (a) the two constituent classical flows; (b) the reduced $x$-momentum equation with justification; (c) the velocity profile $u(y)$.

U moving plate fixed plate u(y) y x centreline gap 2b
Figure 4. Superposition of a linear Couette profile (moving top plate) and a parabolic Poiseuille profile (pressure gradient); $y$ is measured from the centreline, plates at $y=\pm b$.
  1. (a) The two classical flows. (i) Plane Couette flow — shear-driven flow between two plates, one moving; with no pressure gradient the profile is linear, $u=U(1+y/b)/2$. (ii) Plane Poiseuille flow — pressure-driven flow between two stationary plates; the profile is parabolic and symmetric, $u=-\dfrac{1}{2\mu}\dfrac{dp}{dx}(b^2-y^2)$. The present flow is their linear superposition (both are solutions of the same linear equation).
  2. (b) Reduced $x$-momentum equation. The full $x$-Navier–Stokes is $$\rho\Big(\frac{\partial u}{\partial t}+u\frac{\partial u}{\partial x}+v\frac{\partial u}{\partial y}\Big)=-\frac{\partial p}{\partial x}+\mu\Big(\frac{\partial^2 u}{\partial x^2}+\frac{\partial^2 u}{\partial y^2}\Big).$$ Steady $\Rightarrow\partial u/\partial t=0$; fully developed $\Rightarrow\partial u/\partial x=0$, and continuity $\partial u/\partial x+\partial v/\partial y=0$ with $v=0$ at both walls then forces $v\equiv0$; hence $\partial^2u/\partial x^2=0$ and the convective terms vanish. What remains is a balance of pressure and viscous forces: $$\boxed{0=-\frac{dp}{dx}+\mu\frac{d^2u}{dy^2}\quad\Longleftrightarrow\quad \mu\frac{d^2u}{dy^2}=\frac{dp}{dx}.}$$
  3. (c) Integrate and apply boundary conditions. Because $dp/dx$ is constant, integrate twice: $$u(y)=\frac{1}{2\mu}\frac{dp}{dx}\,y^2+C_1 y+C_2 .$$ With $y$ from the centreline, the no-slip conditions are $u(-b)=0$ (fixed lower plate) and $u(+b)=U$ (moving upper plate). Solving for $C_1,C_2$, $$\boxed{u(y)=\frac{1}{2\mu}\frac{dp}{dx}\big(y^2-b^2\big)+\frac{U}{2}\Big(1+\frac{y}{b}\Big).}$$ The first term is the symmetric parabolic (Poiseuille) contribution — note it is negative for a favourable $dp/dx\lt0$, i.e. it adds forward flow — and the second is the linear (Couette) contribution from the moving plate.
Question 4 — results
ItemResult
Constituent flowsplane Couette + plane Poiseuille
Reduced equation$\mu\,d^2u/dy^2=dp/dx$
Velocity profile$u(y)=\dfrac{1}{2\mu}\dfrac{dp}{dx}(y^2-b^2)+\dfrac{U}{2}\big(1+\tfrac{y}{b}\big)$