Bernoulli-induced errors in altimeters

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SUMMARY

The discussion centers on the impact of Bernoulli-induced errors on altimeter readings in aircraft during gusty conditions. It is established that the static ports on aircraft are designed to minimize the influence of airflow on pressure readings, yet sudden changes in wind direction can still affect altitude measurements. The relationship between pressure and altitude remains consistent, as both static pressures in moving and still air at the same altitude are equal. However, a 20mph wind can create a velocity pressure of approximately 0.4 mm HG, translating to an altitude error of about 17 feet, which may be noticeable under certain conditions.

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  • Understanding of Bernoulli's principle and its applications
  • Knowledge of aircraft altimeter functionality
  • Familiarity with atmospheric pressure concepts
  • Basic principles of aerodynamics and airflow dynamics
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  • Explore the effects of atmospheric pressure changes on flight performance
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Aerospace engineers, pilots, meteorologists, and aviation safety professionals will benefit from this discussion, particularly those interested in the accuracy of altitude readings in varying weather conditions.

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When an aircraft flies through things like updrafts, downdrafts, horizontal gusts and so on, does the velocity change produce Bernoulli effects that push the displayed altitude up or down wrt the correct altitude? If so, how much of a practical problem is it?

(By velocity change I mean the air velocity, of course, and not the plane's)
 
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Normally the static port(s) on an aircraft are located so that the speed of flow across the port does not significantly affect the static pressure sensed by the port(s), located inside the boundary layer(s). A gusting wind with a component of wind perpendicular to a static port would affect the reading. If the gust is momentary, the reading will only be affected momentarily. If there is a change in wind direction, eventually the aircraft will react to a crosswind by changing direction, so that there isn't a crosswind, assuming the aircraft is not being kept in a yawed state (a constant crosswind component).
 
Yes, there would be artifacts from how the air flow interacts with the instrument, as you describe. Those would be errors in the pressure measurement which would indirectly translate to altitude errors.

But my question was more about the relation between pressure and altitude, assuming that we can somehow measure the pressure very accurately. Would the dynamics of the gusting wind alter the relation between pressure and altitude to a degree that might matter, considering that fast moving air should have a lower pressure than stationary air at the same altitude and temperature?

For example, consider two balloons that are at the same altitude. One balloon is floating in still air and the other is being carried along in a stream of air. Would their altimeters show different pressures? If so, the pressure on the moving one would be wrongly interpreted as a lower altitude. Or... is this a naive and wrong application of Bernoulli?
 
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Although altimeters may self-calibrate based on GPS, I doubt typical altimeters take weather into account. Rather than compare a still versus moving stream of air, consider still air in the middle of a high pressure zone versus still air in the middle of a low pressure zone. I don't know how altimeters compensate for weather.
 
rcgldr said:
I don't know how altimeters compensate for weather.
They don't. You have to zero the altimeter just before you take off and then believe what the meteorologists tell you about any changes in atmospheric pressure with time. Any other information like radar and observations of your plane from the ground could help you when you are up there.
 
Swamp Thing said:
...considering that fast moving air should have a lower pressure than stationary air...

For example, consider two balloons that are at the same altitude. One balloon is floating in still air and the other is being carried along in a stream of air. Would their altimeters show different pressures? If so, the pressure on the moving one would be wrongly interpreted as a lower altitude. Or... is this a naive and wrong application of Bernoulli?
It's a wrong interpretation of Bernoulli (or rather, this has nothing to do with Bernoulli's principle); the two static pressures are equal.
 
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Doing some quick math on this, a 20mph wind has a velocity pressure of 0.4 mm HG, or about 17' of altitude. So the effect of a sudden gust would be enough to notice if the altimeter wasn't damped, but still pretty small unless you're getting up into the jet stream.
 
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