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Fluid Flow - Reynolds Number
Solid objects like cars, boats and airplanes, things that move,
experience drag because of the flow of fluid around them. When the
fluid is air, the force of drag is called aerodynamic drag
or air resistance. When the fluid is water, the force of drag is
called hydrodynamic drag. The force of drag produced
depends on the way fluid flows around the object. Whether the fluid
is air, water or something else, there are two types of flow,
laminar and turbulent.
Laminar flow ocurrs when the air stream around the
object is smooth. Using a model car as an example, the speed of the
air next to it is close to the speed of the car because air sticks
to the car a little. This syrup-like property of air (or any fluid)
is called viscousity. For air it is very low, but it is
there. A little further from the car the air's speed drops smoothly
to zero. Under these conditions, the aerodynamic drag is low.
Turbulent flow occurs when the air stream breaks up and
causes little whirlwind currents next to, say, a rocket's skin. The
speed of the air drops suddenly just off of its surface, a
condition called wind shear. These conditions cause much
higher aerodynamic drag. In water, this effect is called
cavitation because air is squeezed out of the water due to the
turbulant change in pressure.
Fortuneately, the air flow over many hobby models is nearly all
laminar. We know this because of an indicator called the
Reynolds number. Its symbol is RN.
RN |
Reynolds Number |
p |
is the weight-density of the fluid in oz/in3 |
u |
is the dynamic viscosity of the fluid in ozs/in2 |
v |
is the velocity of the fluid flow in in/s |
L |
the distance over which the air is in contact with the object,
most often its length in inches |
g |
the acceleration of gravity in inches per second squared |
For a Grand Prix car body, v is at most 15 feet/sec (180 in/s)
and L is at most 7 inches, so RN is at most 54,308 on the official
AWANA track. RN is an indicator because if it is under 100,000 then
the flow will be laminar. If it is over 1,000,000 it will be
turbulent. In between, in the transition range, it can be
either.
Symbol or Term |
Value |
v (guess speed of vehicle) |
_______ in/s |
L (measure length of vehicle) |
_______ in |
vL (multiply v and L) |
_______ in2/s |
Symbol or Term |
AIR at ~60 degrees F and 1 atm |
WATER |
p |
0.0007129 oz/in3 |
0.577 oz/in3 |
u |
0.00000004284 ozs/in2 |
0.00002325466 ozs/in2 |
g (at sea level) |
386.088 in/s2 |
386.088 in/s2 |
p/ug |
43.10 s/in2 |
64.27 s/in2 |
Results |
RN in air |
RN in water |
RN (multiply vL and p/ug) |
_______ |
_______ |
Laminar: RN < 100,000 |
[_]Yes or [_]No |
[_]Yes or [_]No |
Turbulant: RN > 1,000,000 |
[_]Yes or [_]No |
[_]Yes or [_]No |
Either: 100,000 < RN < 1,000,000 |
[_]Yes or [_]No |
[_]Yes or [_]No |
In the literature, you can find other formulations of Reynolds
Number. Each may have its own limits for the transition region.
This is because the units used in the parameters are on different
scales. For example, the scale length may be in inches, but the
velocity in feet per second. The resulting Reynolds Number will be
smaller from the one calculated above by a factor of 1/12 if the
other units are the same.
Many formulations use kinematic viscosity which is the
dynamic viscosity used above divided by density. That's ug/p in the
symbols used here. That's the inverse of p/ug which was calculaed
above to make the math simpler. So we really used it too!
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