Bernoulli's Equation — Question 8

Section 14-9 · Physics pages 2226–2227

Question 8 Different streamlines can have different Bernoulli constants An inviscid incompressible liquid rotates rigidly in a horizontal plane with velocity vθ = Ωr. The flow is steady. Radial force balance gives dp/dr = ρΩ2r. Let p(0) = pc and compare points at the same height. r vθ = Ωr Circular streamlines have distinct radii and may have distinct energy constants. (a) Find p(r) and the Bernoulli quantity C(r) = p + ρv2/2. (b) Why does variation of C with radius not violate Bernoulli along a streamline? Identify the incorrect prediction from treating C as one universal constant across the flow.
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Question 8 - Solution Different streamlines can have different Bernoulli constants r vθ = Ωr (a) Derivation and calculation dp dr = ρΩ2r ⇒p(r) −pc = Z r 0 ρΩ2r′ dr′. p(r) = pc + 1 2ρΩ2r2 . C(r) = p + 1 2ρv2 = pc + ρΩ2r2 . (b) Result and interpretation Each streamline has fixed radius r, so dC ds streamline = 0, dC dr = 2ρΩ2r̸ = 0. A universal cross-streamline constant would incorrectly imply dp dr = −ρvdv dr = −ρΩ2r, opposite to the required radial pressure gradient. Physical check The flow has vorticity 2Ω; Bernoulli along each circular streamline does not require one constant for all circles.

Question 8

Different streamlines can have different Bernoulli constants

An inviscid incompressible liquid rotates rigidly in a horizontal plane with velocity vθ=Ωrv_\theta=\Omega r. The flow is steady. Radial force balance gives dp/dr=ρΩ2rdp/dr=\rho\Omega^2r. Let p(0)=pcp(0)=p_c and compare points at the same height.

Diagram shown in the original SVG worksheet.

  1. Find p(r)p(r) and the Bernoulli quantity C(r)=p+ρv2/2C(r)=p+\rho v^2/2.

  2. Why does variation of CC with radius not violate Bernoulli along a streamline? Identify the incorrect prediction from treating CC as one universal constant across the flow.

Question 8 - Solution

Different streamlines can have different Bernoulli constants

Diagram shown in the original SVG worksheet.

(a) Derivation and calculation

dpdr=ρΩ2r⇒p(r)−pc=∫0rρΩ2r′dr′.\frac{dp}{dr}=\rho\Omega^2r\Rightarrow p(r)-p_c=\int_0^r\rho\Omega^2r^{\prime}\,dr^{\prime}.p(r)=pc+12ρΩ2r2.\boxed{p(r)=p_c+\tfrac12\rho\Omega^2r^2}.C(r)=p+12ρv2=pc+ρΩ2r2.\boxed{C(r)=p+\tfrac12\rho v^2=p_c+\rho\Omega^2r^2}.

(b) Result and interpretation

Each streamline has fixed radius rr, sodCds|streamline=0,dCdr=2ρΩ2r≠0.\left.\frac{dC}{ds}\right|_{\mathrm{streamline}}=0,\qquad\frac{dC}{dr}=2\rho\Omega^2r\ne0.A universal cross-streamline constant would incorrectly implydpdr=−ρvdvdr=−ρΩ2r,\frac{dp}{dr}=-\rho v\frac{dv}{dr}=-\rho\Omega^2r,opposite to the required radial pressure gradient.\text{opposite to the required radial pressure gradient}.

Physical check

The flow has vorticity 2Ω2\Omega; Bernoulli along each circular streamline does not require one constant for all circles.