Exercises

1. Fluid flows between two non-parallel plane walls, towards the intersection of the planes, in such a manner that if $x$ is measured along a wall from the intersection of the planes then $U(x)=-U_0/x$ , where $U_0$ is a positive constant. Verify that a solution of the boundary layer equation (8.35) can be found such that $\psi$ is a function of $y/x$ only. Demonstrate that this solution yields
   $$\frac{u(x,y)}{U(x)} = F\left[\left(\frac{U_0}{\nu}\right)^{1/2}\,\frac{y}{x}\right],$$
   where $u=\partial\psi/\partial y$ , and
   $$F'' - F^{\,2} = -1,$$
   subject to the boundary conditions $F(0)=0$ and $F(\infty)=1$ . Verify that
   $$F(z) = 3\,\tanh^2\left(\alpha+\frac{z}{\sqrt{2}}\right)-2$$
   is a suitable solution of the previous differential equation, where $\tanh^2\alpha =2/3$ .

2. A jet of water issues from a straight narrow slit in a wall, and mixes with the surrounding water, which is at rest. On the assumption that the motion is non-turbulent and two-dimensional, and that the approximations of boundary layer theory apply, the stream function satisfies the boundary layer equation
   $$\nu\,\frac{\partial^{\,3}\psi}{\partial y^{\,3}}-\frac{\partial\p... ...rtial\psi}{\partial y}\,\frac{\partial^{\,2}\psi}{\partial x\,\partial y} = 0.$$
   Here, the symmetry axis of the jet is assumed to run along the $x$ -direction, whereas the $y$ -direction is perpendicular to this axis. The velocity of the jet parallel to the symmetry axis is
   $$u(x,y)= -\frac{\partial\psi}{\partial y},$$
   where $u(x,-y)=u(x,y)$ , and $u(x,y)\rightarrow 0$ as $y\rightarrow\infty$ . We expect the momentum flux of the jet parallel to its symmetry axis,
   $$M = \rho\int_{-\infty}^{\infty}u^{\,2}\,dy,$$
   to be independent of $x$ .

   Consider a self-similar stream function of the form

   $$\psi(x,y)=\psi_0\,x^{\,p}\,F(y/x^{\,q}).$$
   Demonstrate that the boundary layer equation requires that $p+q=1$ , and that $M$ is only independent of $x$ when $2\,p-q=0$ . Hence, deduce that $p=1/3$ and $q=2/3$ .

   Suppose that

   $$\psi(x,y)=-6\,\nu\,x^{\,1/3}\,F(y/x^{\,2/3}).$$
   Demonstrate that $F(z)$ satisfies
   $$F''' +2\,F\,F'' + 2\,F'^{\,2} = 0,$$
   subject to the constraints that $F'(-z)=F'(z)$ , and $F'(z)\rightarrow 0$ as $z\rightarrow\infty$ . Show that
   $$F(z)=\alpha\,\tanh(\alpha\,z)$$
   is a suitable solution, and that
   $$M= 48\,\rho\,\nu^{\,2}\,\alpha^{\,3}.$$

3. The growth of a boundary layer can be inhibited by sucking some of the fluid through a porous wall. Consider conventional boundary layer theory. As a consequence of suction, the boundary condition on the normal velocity at the wall is modified to $v(x,0)=-v_s$ , where $v_s$ is the (constant) suction velocity. Demonstrate that, in the presence of suction, the von Kármán velocity integral becomes
   $$\nu\left.\frac{\partial u}{\partial y}\right\vert _{y=0} = U^{\,2}\,\frac{d\delta_2}{dx} + U\,\frac{dU}{dx}\,(\delta_1+2\,\delta_2) + U\,v_s.$$
   Suppose that
   $$u(x,y) = U(x)\left\{\begin{array}{lcl} \sin(\alpha\,y)&\mbox{\hsp... ...0\leq y\leq \pi/(2\,\alpha)\\ [0.5ex] 1&&y>\pi/(2\,\alpha) \end{array}\right.,$$
   where $\alpha=\alpha(x)$ . Demonstrate that the displacement and momentum widths of the boundary layer are

   $$\delta_1 =(\pi/2-1)\,\alpha^{\,-1},$$

   $$\delta_2 =(1-\pi/4)\,\alpha^{\,-1},$$

   
   
   respectively. Hence, deduce that
   $$\frac{\nu\,(\pi/2-1)^2}{\delta_1} = U\,(1-\pi/4)\,\frac{d\delta_1}{dx} + \frac{dU}{dx}\,\delta_1+(\pi/2-1)\,v_s.$$

   Consider a boundary layer on a flat plate, for which $U(x) = U_0$ . Show that, in the absence of suction,

   $$\delta_1 = (\pi/2-1)\left(\frac{8}{4-\pi}\right)^{1/2}\left(\frac{\nu\,x}{U_0}\right)^{1/2},$$
   but that in the presence of suction
   $$\delta_1 = \frac{(\pi/2-1)\,\nu}{v_s}.$$
   Hence, deduce that, for a plate of length $L$ , suction is capable of significantly reducing the thickness of the boundary layer when
   $$\frac{v_s}{U_0}\gg \frac{1}{{\rm Re}^{1/2}},$$
   where ${\rm Re} = U_0\,L/\nu$ .