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A static vent separated from the pitot head is shown in Figure 2. There is usually some place on the airframe, usually on the side of the fuselage, where true or nearly true static pressure is obtained over the whole speed range of the aircraft. A flat metal plate is fitted at this position, the Figure 2.
A similar vent is positioned on the opposite side of the fuselage and the two are interconnected for transmission of static pressure to the instruments so that errors 2 produced by yawing are largely eliminated. Errors produced when side-slipping or yawing are reduced.
High Speed Probes The shock waves associated with flight at high mach numbers can produce significant errors in pressure sensed by a static vent. The choice of location for a probe, or vent, is dependent Figure 2. Typical locations are: ahead of a wing tip, under a wing, ahead of the vertical stabilizer tip, at the side of the fuselage nose section, and ahead of the fuselage nose section. Manoeuvre-induced errors are caused by short-term fluctuations of pressure at the static vents and delays in the associated pipelines transmitting pressure changes to the instruments.
Even servo altimeters and air data computer systems suffer from this type of error as they utilize the same static vents as the simple pressure instruments. Change in angle of attack, and turbulence due to lowering or raising flaps and landing gear are the prime causes of the error-producing changes in airflow over the static vents. Most commonly, manoeuvre-induced error appears as a marked lag in pressure instrument indications.
The errors are usually more significant during changes of pitch attitude than during yawing or rolling movements so that the worst effects are at the start of the climb or descent and on levelling out. Overshooting referred to as go-around and flight in rough air are particularly vulnerable.
The errors are unpredictable both in size and in sense so that pressure instruments cannot be relied upon to indicate accurate instantaneous values or accurate rates of change. Discoverany specific books that you want to read online today.
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