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Pressure in fluids can be thought of as a form of potential energy,
as described earlier. Kinetic energy in fluids is expressed in terms of flow,
the bulk movement of fluid with a given direction and speed. We must carefully distinguish
between fluid flow and fluid velocity,
which are often confused. Flow () refers to the volume of fluid passing a
particular location per unit of time; its SI units are meter cubed per second, but
it is more commonly measured in milliliters per second or liters per minute. Fluid
velocity (U) is simply the speed of the fluid at a particular point in space, measured
in meters per second. By analogy, imagine a multilane freeway: the speed (velocity)
of individual cars may vary depending on the lane; the flow is the number of cars
passing a point per minute. The potential energy of pressure can be converted into
the kinetic energy of flow; for example, the hydrostatic pressure generated by gravity
acting on a vertical column of liquid can be transformed into flow by opening a valve
at the bottom of the column. Pressure and flow can also change independently. With
the human
Water | Electricity | Energy |
---|---|---|
Squirt gun | Static electric spark | High pressure, low flow, low energy |
Garden hose | House current | Moderate pressure, moderate flow, moderate energy |
|
Car battery | Low pressure, moderate flow, moderate energy |
River flood |
|
Low pressure, huge flow, huge energy |
Fire hose | High-tension wires | High pressure, high flow |
|
Lightning | High pressure, high flow |
A pressure gradient exerts a force on the fluid, and the fluid
tends to accelerate in the direction of decreasing
pressure. Pressure gradient is only one of the forces that commonly act on fluids;
other forces include gravity (discussed earlier) and viscous force or friction.
If these other forces are negligible and the fluid is incompressible (i.e., a liquid
with constant density), the equation of motion (F = ma) can be integrated
to yield
P + ½ρU2
= P0
(5)
where P is pressure, ρ is fluid density, U is the magnitude of the fluid velocity,
and P0
is a constant called the stagnation pressure
(see Appendix 5
). This form
of the Bernoulli equation tells us that as velocity
increases in a frictionless flow, pressure decreases and vice versa. This concept
resolves the common misconception that pressure always decreases in the direction
of flow. For example, in the flow inside a tube (a pipe or a large vein) of gradually
increasing diameter, fluid velocity (U) decreases in the downstream direction as
the diameter and cross-sectional area of the tube increase. As U decreases, Equation
5 tells us that P actually increases in the direction of flow. This example again
shows the relationship of potential and kinetic energy in fluids: as the kinetic
energy of this tube flow decreases (U2
falls) in the flow direction, the
potential energy increases (P rises) by an equal amount. The total energy remains
constant because we have assumed no friction.
Flow can be determined by knowing the average velocity of the fluid across the tube. In laminar flow, Figure 30-16A , the velocity profile is distributed such that the highest velocity is in the center and the fluid at the edges is virtually stationary. In turbulent flow, the velocity profile is "flattened" ( Fig. 30-16B ). Some monitors measure flow directly, but most measure flow indirectly, by either pressure or velocity measurements.
The Bernoulli equation applies to a specific subset of flow parameters as listed earlier. Many flows important to anesthesiologists do not follow the Bernoulli equation. Most commonly, the flow that we desire to measure is not laminar but turbulent. The transition from laminar
Figure 30-16
Laminar and turbulent flow. In a smooth-walled tube
at low flow rates (i.e., small pressure gradients), the flow rate is laminar; that
is, flow moves smoothly in concentric circles, with the centermost area having the
greatest flow velocity and the area nearest the wall of the tube being virtually
stationary. As the flow rate (and pressure gradient) increases, the flow transitions
from laminar to turbulent. Instead of a neatly ordered flow, the velocities are
more randomly distributed, energy is dissipated as heat, and the energy needed for
a given flow rate increases. Many factors govern this transition, including size
of the tube, viscosity of the fluid, flow rate, and pressure gradient. These factors
are combined in determination of the Reynolds number (see Appendix
5
).
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