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Random Error
In the specific case of wind tunnel experiments,
random error can be addressed by simply taking
lots of data. As one might imagine, the
larger the sample size (more data points), the
lower the random error. In the limiting
case, as the sample size goes to infinity,
random errors will go to zero. The
elimination of random error is a good thing -
though, often times extreme pursuit of this goal
adds costs to the test and can reach a point of
diminishing returns.
A common theme raised by wind tunnel critics
is that the data produced in a tunnel is not
"real world". As support of this
assertion, "real world" data is provided that is
contrary to the conclusions drawn based on wind
tunnel data. Unfortunately, the problem
with most "real world" tests is that they lack
control of all relevant variables (primarily
ambient wind) and they also lack a sufficient
number of trials to reduce random errors.
If a field test is conducted properly,
though, the results should correlate with wind
tunnel tests. This has been demonstrated
in the academic literature:
Validation of a Mathematical
Model for Road Cycling Power
J.Martin, D.Milliken, J.Cobb, K.McFadden,
A.Coggan
Journal of Applied Biomechanics, 1998, 14,
276-291
http://www.humankinetics.com/products/journals/showarticle.cfm?articleid=3751&journalid=JAB
In order to generate statistical confidence
in the test and the results, random error needs
to be addressed. In a wind tunnel, this
means a sufficiently long sample period or
sufficiently high sample rate. In a field
test, this means many runs over the test course
(on the order of 16+ runs - depending on the
magnitude of the effect one is trying to
detect), which takes personnel time.
Systematic Errors
At the root of systematic error during a wind
tunnel test is the instrumentation used to
measure the relevant variables of axial force
(F), air density (rho), air speed (u). In
a nutshell axial force (or drag at 0 degree
yaw), is defined as (Cd/Cx is axial force
coefficient and A is projected area):

Most tunnel data is presented as an axial force
at a normalized tunnel speed of 30 mph or some
other constant value (this corrects for the
slight variations in tunnel speed during the
actual trial - 30.1 mph or 29.9 mph, etc...).
Therefore, the presented data is really a
function of the tunnel determined product "CxA".
As shown above, CxA is dependent on F, rho, and
u. Physical instruments must measure these
quantities, and each of these instruments will
have their own contribution to the CxA term.
An uncertainty analysis is a common exercise
used to explore what is primarily responsible
for the error of the measurement. In
essence, the total uncertainty is the
square-root of the sum of the squares of each of
the individual instruments (that equation above
that has all the partial derivative terms).

So, if we continue the uncertainty exercise
we find that for each of the terms:
A note on one of the assumptions used in the
equations above - it is assumed that lab
quality, precision instruments are being used
that have been calibrated to be accurate to +/-
0.1 % of a full-scale value. So, if an
instrument was designed and calibrated to
measure a 100 lb load and exhibits a +/- 0.1% of
full-scale value, the uncertainty of that
instrument would be +/- 0.1 lbs.
Now, if we plug these terms back into our
original equation, and investigate a typical
wind tunnel run done at 25 mph, we can see what
component (air density, tunnel speed, or the
force) of our instrumentation is driving the
total uncertainty in the final results:

As the grayed/highlighted boxes show above, the
force measurement term is several orders of
magnitude larger than the air density and tunnel
speed terms. Thus, it is reasonable to
conclude that that the primary contributor to
tunnel error is typically the wind tunnel force
measurement system.
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