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#9
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Yikes, my head hurts!
Static pressure is simply that. The static pressure of the ambient air around you. A good aircraft static system should give you the same value for any given ambient pressure (ie altitude) no matter how fast your glider is going. Dynamic pressure is the pressure due to velocity and it varies by the square of the velocity (ie twice the velocity = four times the pressure). The ASI measures the difference between the dynamic (pitot) pressure and the static pressure to give velocity. Keep in mind that the static pressure at the pitot and at the static port are the same and cancel each other out in the equation (unless like most of us you have a horrible static system). The difference between the pressure at the TE probe and static pressure should be the same as the dynamic pressure but of opposite sign. Again static pressure at both locations is the same so it cancels. I have driven many miles with an automobile test rig consisting of a pitot, a static and a TE probe connected to a pair of side by side U-tube water manometers. The manometers share the same static and one uses the pitot signal while the other uses the TE signal. A properly calibrated TE probe will cause exactly the same pressure difference as the pitot, just with the opposite sign. The mounting bracket for the probes hung out way in front of the car to get clean air for the testing. I must say it got quite a few stares. In practice I usually build TE probes to overcompensate slightly to make up for poor static systems. The probes are easy for the user to tame down slightly and they can be tailored by the individual pilot to match their preference and sailplane. |
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