Steve MacDonald wrote;
Quoted message said:Aerodynamic resistance doesn't necessarily increase by a factor of 4 with an increase in
speed. It really can't be calculated without actual testing, using a full-sized model or
actual working vehicle. This is because different airframes have variations in how well they
perform at certain speeds. Some airframes have a terminal velocity that is lower than others,
because the airflow becomes turbulent enough at that speed to greatly raise the drag. Other
designs might allow a smooth airflow to be maintained at much greater speeds. Some designs
might have poor airflow characteristics at lower speeds, but when pushed faster the airflows
might smooth out into more laminar patterns.
Steve
The difference between airplanes (Cd's under .1) and bluff bodies like unfaired bicycles (Cd's
from ~.5 to about .9) is that almost all of the drag on airplanes is from skin friction, and
almost all of the drag on unfaired bicycles drag is due to pressure drag.
Cd's are just a measure of the streamlining of any object, per unit of frontal area. The lower
the Cd, the more streamlined the object.
Airplanes also have much higher speeds, and complicated laminar/turbulent flow control problems
under various yaws, lifts, etc. In general, a much more complicated problem than the normal
turbulent and separating air flow of unfaired bicycles.
The range of speeds of interest for bicycle aero drag calculation's is also much slower at
20-35 MPH, and in a stable Cd range.
Cd's of various objects can change based on speed, size, and fluid viscosity (which the
dimensionless "Reynolds number" describes) and suddenly drop by a factor of four over a very
small range of velocities, as air is tripped into turbulence and reduces the separated area
(low pressure) behind the object.
I've never seen bicycle Cd's change over the normal range of wind tunnel velocities though, so
the aero drag force does scale with the velocity squared for the normal range of interest.
Rich Pinto
Bacchetta Bicycles