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Exact solutions: Couette, Poiseuille and Stokes' first problem
The flows in which the nonlinear term vanishes, solved exactly and checked against the full equations.
The Navier-Stokes equations have few exact solutions, and most of them share a trick: the nonlinear term vanishes identically. For a unidirectional flow \(\mathbf{u} = (u(y,t),0,0)\), incompressibility holds automatically and \((\mathbf{u}\cdot\nabla)\mathbf{u} = u\,\partial_x u\,\mathbf{e}_x = 0\). The \(y\) and \(z\) components of the momentum equation give \(\partial_y p = \partial_z p = 0\), and the \(x\) component \[ \frac{\partial u}{\partial t} = -\frac{1}{\rho}\frac{\partial p}{\partial x} + \nu\frac{\partial^2 u}{\partial y^2} \] shows \(\partial_x p\) depends only on time. So \(\partial_x p = -G(t)\), and what is left is a linear heat equation.
Couette flow (Couette, 1890). Fluid between a fixed plate at \(y = 0\) and a plate at \(y = h\) moving at speed \(U\), with no pressure gradient. Steady flow needs \(u'' = 0\), and no-slip gives \(u = Uy/h\). The shear stress \(\mu U/h\) is the same at every height. Plane Poiseuille flow. Both plates fixed, a pressure gradient \(G\) driving the fluid: \(\mu u'' = -G\), \(u(0) = u(h) = 0\), so \[ u = \frac{G}{2\mu}\,y(h-y), \qquad Q = \int_0^h u\,dy = \frac{Gh^3}{12\mu}. \] A parabola, fastest in the middle, with mean speed two thirds of the maximum. In a round pipe of radius \(a\) the same reasoning in cylindrical coordinates gives the Hagen-Poiseuille profile (Hagen 1839, Poiseuille 1840) \(u = \frac{G}{4\mu}(a^2 - r^2)\) and flow rate \(Q = \frac{\pi G a^4}{8\mu}\). The fourth power of the radius is why narrowing an artery by a fifth cuts the flow by more than half.
Stokes' first problem (Stokes, 1851; often called Rayleigh's problem). Fluid at rest above a plate that suddenly starts moving at speed \(U\): solve \(u_t = \nu u_{yy}\), \(u(0,t) = U\), \(u(y,0) = 0\). There is no length scale in the problem except \(\sqrt{\nu t}\), so the solution depends on \(\eta = y/(2\sqrt{\nu t})\) alone, and \[ u = U\operatorname{erfc}\!\left(\frac{y}{2\sqrt{\nu t}}\right). \] The disturbance spreads a distance of order \(\sqrt{\nu t}\): viscosity diffuses momentum, slowly. If the plate oscillates instead (Stokes' second problem), \(u = Ue^{-ky}\cos(\omega t - ky)\) with \(k = \sqrt{\omega/(2\nu)}\).
A genuinely two-dimensional example is the decaying Taylor-Green vortex (1937), \[ \mathbf{u} = (\sin x\cos y,\ -\cos x\sin y)\,e^{-2\nu t}, \qquad p = \tfrac14(\cos 2x + \cos 2y)\,e^{-4\nu t}. \] Here the nonlinear term does not vanish, but it is a gradient and is balanced exactly by the pressure. Checking such a solution is a matter of differentiating and substituting, and it is worth doing once by hand.
Picture it: the velocity profile across a channel is a straight line when a wall drags the fluid and a parabola when pressure pushes it; they add, because the equation for them is linear. Think it: every exact solution here lives in a subspace where \((\mathbf{u}\cdot\nabla)\mathbf{u}\) is zero or a gradient, so Navier-Stokes collapses to a heat equation. Such solutions say nothing about the hard nonlinear questions, which is precisely why they can be solved.
ਕੰਮ ਉਦਾਹਰਨ · y'' = -2
Y'' = -2
ਕਦਮ ਦਰ ਕਦਮ
- \frac{d^{2}}{d x^{2}} y{\left(x \right)} = -2
The differential equation.
- \text{order } 2
Order 2: the highest derivative present.
- \text{Undetermined coefficients}
Solve the homogeneous part from the characteristic equation, then guess a particular solution shaped like the right-hand side.
- r^{2} = 0
Characteristic equation of the homogeneous part (substitute y = e^{rx}).
- r = 0\ (\times 2)
Its roots.
- y{\left(x \right)} = C_{1} + C_{2} x - x^{2}
General solution (C₁, C₂ … are arbitrary constants).
- \checkmark
Verified: substituting the solution back into the equation gives 0.
ਜਵਾਬ ਦਿਓ
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ਇੱਥੇ ਵਰਤੇ ਨਿਸ਼ਾਨ
ਕਿਸੇ ਵੀ ਨਿਸ਼ਾਨ ਨੂੰ ਦਬਾਉ, ਜਿਸ ਵਿੱਚ ਪੂਰੀ ਪਰਿਭਾਸ਼ਾ, ਇੱਕ ਤਸਵੀਰ ਅਤੇ ਹਰ ਅੱਖਰ ਦਾ ਅਰਥ ਹੈ ।
ਕਿਵੇਂ: Exact solutions: Couette, Poiseuille and Stokes' first problem
- Guess the form: u = (u(y, t), 0, 0) for flow between plates, u = u(r) along a pipe.
- Check the nonlinear term vanishes and read off that the pressure gradient is a constant -G.
- Solve the resulting ODE (or heat equation) and impose no-slip on each wall.
- Verify: substitute back into both equations, then integrate the profile for the flow rate.
ਲੋਕ ਪੁੱਛਦੇ ਹਨ
Why does Poiseuille flow stop being observed at high speed?
It remains an exact solution, but disturbances of finite size can knock it into turbulence. In a pipe this typically happens above a Reynolds number of about 2000, even though the flow is stable to infinitesimal disturbances in every computation so far, and very careful experiments keep it laminar much longer.
What is erfc?
The complementary error function, erfc(s) = (2/sqrt(pi)) times the integral of exp(-r^2) from s to infinity. It falls from 1 at s = 0 to 0 as s grows, the shape of heat spreading from a suddenly heated wall.
What do I need before starting fluid dynamics?
Multivariable calculus (divergence, curl, the divergence and Stokes theorems), linear algebra (symmetric matrices and eigenvalues) and partial differential equations (the heat and Laplace equations). The last lessons also use Sobolev spaces, which are introduced where they are needed.
What are the Navier-Stokes equations in one sentence?
Newton's second law for each particle of a viscous incompressible fluid: acceleration equals the pressure force plus viscous diffusion of momentum, with the constraint that the velocity field is divergence-free.
Why is two-dimensional flow easier than three-dimensional flow?
In 2D the vorticity is a scalar that is only carried and diffused, so its maximum never grows; in 3D vortex lines can be stretched, which amplifies vorticity, and no known bound rules out unlimited growth.
Is this course physics or mathematics?
Both, in order. The first half derives the equations from physical principles and solves classical flows; the second half treats the equations as mathematical objects and studies which of their properties can be proved.
ਹੋਰ ਵਿੱਚ Fluid Dynamics
The continuum hypothesis and fieldsEulerian and Lagrangian descriptions, the material derivativeKinematics: streamlines, pathlines and streaklinesConservation of mass, the continuity equation and incompressibilityThe stream function and two-dimensional incompressible flowVorticity, circulation and Kelvin's circulation theoremThe stress tensor and Cauchy's momentum equationHydrostatics and pressureThe Euler equations and Bernoulli's theoremPotential flow and the Laplace equationViscosity, Newtonian fluids and the Navier-Stokes equationsDimensional analysis, the Reynolds number and the scaling symmetryStokes flow at low Reynolds numberBoundary layers