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Trailing cone

From Wikipedia, the free encyclopedia
A Boeing 787-8 during a test flight with a trailing cone attached to the vertical stabilizer

A trailing cone (also a trailing static cone or, incorrectly, a trailing wire) is an aviation calibration tool first developed and tested in the 1950s and 1960s as a simple means of determining or calibrating the static pressure (altitude reporting) of an aircraft's pitot-static system.[1] It does this by giving an accurate measurement of the ambient atmospheric pressure (static pressure) well clear of the aircraft's fuselage.[2] The trailing cone system typically trails at least one fuselage length behind the aircraft via a high-strength cable containing a tube or attached to a tube to cone or similar stabilizing device at the end. Static pressure is measured forward of the cone by several static ports.[3] The cone stabilizes and aligns the ports relative to the freestream airflow.[4]


Other precision static pressure measurement methods in test flight

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As stated in FAA Advisory Circular AC 91-85A:

  • Precision tracking radar in conjunction with pressure calibration of atmosphere at test altitude
  • Chase aircraft
  • Any other method acceptable to the approving authority

See also

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References

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  1. "Home - FUTEK Advanced Sensor Technology V2".
  2. "Flight Test Equipment".
  3. "Trailing cone".
  4. "Design and Development of a Self-Contained Trailing Static Pressure Measurement System Prototype" (PDF). faculty.washington.edu.
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