What is the Blood Pressure Difference in a Narrowed Artery Segment?

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SUMMARY

The discussion focuses on calculating the blood pressure difference between a normal artery segment and a narrowed segment due to arteriosclerotic plaque. The normal blood speed is 0.13 m/s, and the narrowed segment has one-fifth the cross-sectional area. Using the continuity equation and Bernoulli's equation, the pressure difference is determined to be ΔP = -12 * density of blood * v1², indicating a decrease in static pressure in the narrowed segment.

PREREQUISITES
  • Understanding of Bernoulli's equation for incompressible flow
  • Familiarity with the continuity equation in fluid dynamics
  • Knowledge of Newtonian viscous fluids and their properties
  • Basic concepts of blood viscosity and density
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  • Study the application of Bernoulli's equation in fluid dynamics
  • Learn about the continuity equation and its implications in blood flow
  • Research the properties of Newtonian fluids and their relevance in biological systems
  • Explore the effects of arteriosclerosis on blood flow and pressure
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Medical professionals, biomedical engineers, and students studying cardiovascular physiology will benefit from this discussion, particularly those interested in fluid dynamics and its applications in human health.

texasgrl05
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not sure where to begin...

The blood speed in a normal segment of a horizontal artery is 0.13 m/s. An abnormal segment of the artery is narrowed down by an arteriosclerotic plaque to one-fifth the normal cross-sectional area. What is the difference in blood pressures between the normal and constricted segments of the artery? (See Table 11.1 for appropriate constants.)
 
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Are you sure you don't need the Poiseuille-Hagen (1839) equation...?

Blood is viscous and it can be modeled by a Newtonian viscous fluid.

Daniel.
 
I have no idea what that is. It just says Bournelli's equation
 
Ok.I'm sure it's Daniel Bernoulli.

Use the continuity equation to find the velocity in the other portion of the artery and then Bernoulli's law to find the pressure difference.

Daniel.
 
Bernoullis eqn says that for incompressible flow we have

P1 + Q1 = P2 + Q2

P corresponds to the static pressure
Q is the dynamic pressure

Q = 1/2pv^2

From the continuity equation we have

mdot1 = mdot2

mdot = density*area*velocity

Assuming INCOMPRESSIBLE
density1 = density2 thus

A1*v1 = A2*v2

A2 = A1/5 Thus v2 = 5*v1

Q1 = 1/2*density of blood*v1^2
Q2 = 1/2*density of blood*(5*v1)^2

P1 + Q1 = P2 + Q2

The change in pressure is P2 - P1

P2 - P1 = 1/2*density of blood*(v1^2 - 25v1^2)

delta P = -12*density of blood*v1^2

notice this value is negative thus the static pressure decreases

The pressure drop is simply 12*density of blood*v1^2
 

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