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Next: 2D Potential Flow Up: Incompressible Inviscid Fluid Dynamics Previous: Velocity Potentials and Stream

Exercises

  1. Liquid is led steadily through a pipeline that passes over a hill of height $h$ into the valley below, the speed at the crest being $v$. Show that, by properly adjusting the ratio of the cross-sectional areas of the pipe at the crest and in the valley, the pressure may be equalized at these two places.

  2. For the case of the two-dimensional motion of an incompressible fluid, determine the condition that the velocity components
    $\displaystyle v_x$ $\textstyle =$ $\displaystyle a\,x+b\,y,$  
    $\displaystyle v_y$ $\textstyle =$ $\displaystyle c\,x+d\,y$  

    satisfy the equation of continuity. Show that the magnitude of the vorticity is $c-b$.

  3. For the case of the two-dimensional motion of an incompressible fluid, show that
    $\displaystyle v_x$ $\textstyle =$ $\displaystyle 2\,c\,x\,y,$  
    $\displaystyle v_y$ $\textstyle =$ $\displaystyle c\,(a^2+x^2-y^2)$  

    are the velocity components of a possible flow pattern. Determine the stream function and sketch the streamlines. Prove that the motion is irrotational, and find the velocity potential.

  4. A cylindrical vortex in an incompressible fluid is co-axial with the $z$-axis, and such that $\omega_z$ takes the constant value $\omega$ for $r\leq a$, and is zero for $r>a$, where $r$ is a cylindrical coordinate. Show that

    \begin{displaymath}
\frac{1}{\rho}\,\frac{dp}{dr} = \frac{\kappa^2\,r}{a^4},
\end{displaymath}

    where $p(r)$ is the pressure at radius $r$ inside the vortex, and the circulation of the fluid outside the vortex is $2\pi\,\kappa$. Deduce that

    \begin{displaymath}
p(r) = \frac{\kappa^2\,r^2\,\rho}{2\,a^4}+ p_0,
\end{displaymath}

    where $p_0$ is the pressure at the center of the vortex.

  5. Consider the cylindrical vortex discussed in Exercise 5.4. If $p(r)$ is the pressure at radius $r$ external to the vortex, demonstrate that

    \begin{displaymath}
p(r) = -\frac{\kappa^2\,\rho}{2\,r^2}+ p_\infty,
\end{displaymath}

    where $p_\infty$ is the pressure at infinity.

  6. Show that the stream function for the cylindrical vortex discussed in Exercises 5.4 and 5.5 is $\psi(r)=(1/2)\,\omega\,a^2\,\ln(r/a)$ for $r>a$, and $\psi(r)=(1/4)\,\omega\,(r^2-a^2)$ for $r\leq a$.

  7. Consider a volume $V$ whose boundary is the surface $S$. Suppose that $V$ contains an incompressible fluid whose motion is irrotational. Let the velocity potential $\phi$ be constant over $S$. Prove that $\phi$ has the same constant value throughout $V$. [Hint: Consider the identity $\nabla\cdot(A\,\nabla A)\equiv \nabla A\cdot \nabla A +A\,\nabla^2 A$.]

  8. In Exercise 5.7, suppose that, instead of $\phi$ taking a constant value on the boundary, the normal velocity is everywhere zero on the boundary. Show that $\phi$ is constant throughout $V$.

  9. Prove that in the two-dimensional motion of a liquid the mean tangential fluid velocity around any small circle of radius $r$ is $\omega\,r$, where $2\,\omega$ is the value of

    \begin{displaymath}
\frac{\partial v_y}{\partial x}- \frac{\partial v_x}{\partial y}
\end{displaymath}

    at the center of the circle. Neglect terms of order $r^3$.

  10. Show that the equation of continuity for the two-dimensional motion of an incompressible fluid can be written

    \begin{displaymath}
\frac{\partial (r\,v_r)}{\partial r} + \frac{\partial v_\theta}{\partial\theta}=0,
\end{displaymath}

    where $r$, $\theta $ are cylindrical coordinates. Demonstrate that this equation is satisfied when $v_r=a\,k\,r^n\,\exp[-k\,(n+1)\,\theta]$ and $v_\theta=a\,r^n\,\exp[-k\,(n+1)\,\theta]$. Determine the stream function, and show that the fluid speed at any point is

    \begin{displaymath}
(n+1)\,\psi\,\sqrt{1+k^2}/r,
\end{displaymath}

    where $\psi $ is the stream function at that point (defined such that $\psi=0$ at $r=0$).

  11. Demonstrate that streamlines cross at right-angles at a stagnation point in two-dimensional, incompressible, irrotational flow.

  12. Consider two-dimensional, incompressible, inviscid flow. Demonstrate that the fluid motion is governed by the following equations:
    $\displaystyle \frac{\partial\omega}{\partial t} +[\psi,\omega]$ $\textstyle =$ $\displaystyle 0,$  
    $\displaystyle \nabla^2\psi$ $\textstyle =$ $\displaystyle \omega,$  
    $\displaystyle \nabla^2\chi$ $\textstyle =$ $\displaystyle \nabla\omega\cdot\nabla\psi + \omega^2,$  

    where ${\bf v} = {\bf e}_z\times \nabla\psi$, $[A,B] = {\bf e}_z\cdot\nabla A \times\nabla B$, and $\chi = p/\rho+(1/2)\,v^2+{\mit\Psi}$.

  13. For irrotational, incompressible, inviscid motion in two-dimensions show that

    \begin{displaymath}
\nabla q\cdot\nabla q = q\,\nabla^2 q,
\end{displaymath}

    where $q=\vert{\bf v}\vert$.


next up previous
Next: 2D Potential Flow Up: Incompressible Inviscid Fluid Dynamics Previous: Velocity Potentials and Stream
Richard Fitzpatrick 2012-04-27