Question 4.5: Take the velocity field of Example 4.3, with b = 0 for algeb...

Take the velocity field of Example 4.3, with b = 0 for algebraic convenience

u = a(x^2 - y^2)                v = -2axy                     w = 0

and determine under what conditions it is a solution to the Navier-Stokes momentum equations (4.38). Assuming that these conditions are met, determine the resulting pressure distribution when z is “up” (g_x = 0,  g_y = 0,  g_z = -g).

\rho g_x - \frac{\partial p}{\partial x} + \mu \left(\frac{\partial^2 u}{\partial x^2}+\frac{\partial^2 u}{\partial y^2}+\frac{\partial^2 u}{\partial z^2}\right)=\rho \frac{du}{dt}

 

\rho g_y - \frac{\partial p}{\partial y} + \mu \left(\frac{\partial^2 v}{\partial x^2}+\frac{\partial^2 v}{\partial y^2}+\frac{\partial^2 v}{\partial z^2}\right)=\rho \frac{dv}{dt}

 

\rho g_z - \frac{\partial p}{\partial z} + \mu \left(\frac{\partial^2 w}{\partial x^2}+\frac{\partial^2 w}{\partial y^2}+\frac{\partial^2 w}{\partial z^2}\right)=\rho \frac{dw}{dt}                      (4.38)

The Blue Check Mark means that this solution has been answered and checked by an expert. This guarantees that the final answer is accurate.
Learn more on how we answer questions.

• Assumptions: Constant density and viscosity, steady flow (u and v independent of time).

• Approach: Substitute the known (u, v, w) into Eqs. (4.38) and solve for the pressure gradients. If a unique pressure function p(x, y, z) can then be found, the given solution is exact.

• Solution step 1: Substitute (u, v, w) into Eqs. (4.38) in sequence:

\rho (0) – \frac{\partial p}{\partial x} + \mu (2a – 2a + 0)=\rho \left(u\frac{\partial u}{\partial x}+v\frac{\partial u}{\partial y}\right)=2a^2 \rho(x^3+xy^2)

 

\rho (0) – \frac{\partial p}{\partial y} + \mu (0 + 0 + 0)=\rho \left(u\frac{\partial v}{\partial x}+v\frac{\partial v}{\partial y}\right)=2a^2 \rho(x^2 y+y^3)

 

\rho (-g) – \frac{\partial p}{\partial z} + \mu (0 + 0 + 0)=\rho \left(u\frac{\partial w}{\partial x}+v\frac{\partial w}{\partial y}\right)=0

Rearrange and solve for the three pressure gradients:

\frac{\partial p}{\partial x}=-2a^2 \rho(x^3+xy^2)                    \frac{\partial p}{\partial y}=-2a^2 \rho(x^2 y+y^3)                      \frac{\partial p}{\partial z}=-\rho g                     (1)

• Comment 1: The vertical pressure gradient is hydrostatic. (Could you have predicted this by noting in Eqs. (4.38) that w = 0?) However, the pressure is velocity-dependent in the xy plane.

• Solution step 2: To determine if the x and y gradients of pressure in Eq. (1) are compatible, evaluate the mixed derivative,(\partial^2 p/ \partial x  \partial y); that is, cross-differentiate these two equations:

\frac{\partial}{\partial y}\left(\frac{\partial p}{\partial x}\right)=\frac{\partial}{\partial y}[-2a^2 \rho(x^3+xy^2)]=-4a^2 \rho xy

 

\frac{\partial}{\partial x}\left(\frac{\partial p}{\partial y}\right)=\frac{\partial}{\partial x}[-2a^2 \rho(x^2 y+y^3)]=-4a^2 \rho xy

• Comment 2: Since these are equal, the given velocity distribution is indeed an exact solution of the Navier-Stokes equations.

• Solution step 3: To find the pressure, integrate Eqs. (1), collect, and compare. Start with \partial p / \partial x. The procedure requires care! Integrate partially with respect to x, holding y and z constant:

p=\int{\frac{\partial p}{\partial x}dx}|_{y,z}=\int{-2a^2 \rho(x^3+xy^2)dx}|_{y,z}=-2a^2 \rho\left(\frac{x^4}{4}+\frac{x^2 y^2}{2}\right)+f_1(y,z)                       (2)

Note that the “constant” of integration f_1 is a function of the variables that were not integrated. Now differentiate Eq. (2) with respect to y and compare with \partial p / \partial y from Eq. (1):

\frac{\partial p}{\partial y}|_{(2)}=-2a^2 \rho x^2y+\frac{\partial f_1}{\partial y}=\frac{\partial p}{\partial y}|_{(1)}=-2a^2 \rho(x^2y+y^3)

Compare: \frac{\partial f_1}{\partial y}=-2a^2 \rho y^3                    or                  f_1=\int{\frac{\partial f_1}{\partial y}dy}|_{z}=-2a^2 \rho \frac{y^4}{4}+f_2(z)

Collect terms: So far         p=-2a^2 \rho\left(\frac{x^4}{4}+\frac{x^2 y^2}{2}+\frac{y^4}{4}\right)+f_2(z)                            (3)

This time the “constant” of integration f_2 is a function of z only (the variable not integrated). Now differentiate Eq. (3) with respect to z and compare with \partial p / \partial z from Eq. (1):

\frac{\partial p}{\partial z}|_{(3)}=\frac{\partial f_2}{\partial z}=\frac{\partial p}{\partial z}|_{(1)}=-\rho g                           or                  f_2=-\rho gz+C                                        (4)

where C is a constant. This completes our three integrations. Combine Eqs. (3) and (4) to obtain the full expression for the pressure distribution in this flow:

p(x,  y,  z) = -ρgz – \frac{1}{2} a^2 \rho (x^4 + y^4 + 2x^2y^2) + C                            Ans. (5)

This is the desired solution. Do you recognize it? Not unless you go back to the beginning and square the velocity components:

u^2 + v^2 + w^2 = V^2 = a^2(x^4 + y^4 + 2x^2y^2)                      (6)

Comparing with Eq. (5), we can rewrite the pressure distribution as

p + \frac{1}{2} \rho V^2 + pgz = C                       (7)

• Comment: This is Bernoulli’s equation (3.54). That is no accident, because the velocity distribution given in this problem is one of a family of flows that are solutions to the Navier-Stokes equations and that satisfy Bernoulli’s incompressible equation everywhere in the flow field. They are called irrotational flows, for which curl V = ∇ × V ≡ 0. This subject is discussed again in Sec. 4.9.

\frac{p_1}{\rho}+\frac{1}{2}V^2_1+gz_1=\frac{p_2}{\rho}+\frac{1}{2}V^2_2+gz_2 = const                      (3.54)

Related Answered Questions