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Evandenberg (talk | contribs) (Created page with "The static system measures the static pressure. So all influences of airspeed are eliminated. In real life this is however not always easy. Effects from angle of attack, side-...") |
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The static system measures the static pressure. So all influences of airspeed are eliminated. In real life this is however not always easy. Effects from angle of attack, side-slip, flap defection, gear extension, engine power setting and airspeed are present and for the aircraft designer it is not | The static system measures the static pressure. So all influences of airspeed are eliminated. In real life this is however not always easy. Effects from angle of attack, side-slip, flap defection, gear extension, engine power setting and airspeed are present and for the aircraft designer it is not always easy to find a good position for the static port. | ||
Usually the number of static systems are equal to the number of pitot systems. | Usually the number of static systems are equal to the number of pitot systems. |
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