AIRCRAFT COMPRISING A MEASURING PROBE AND METHOD FOR DETERMINING FLIGHT PARAMETERS OF SUCH AN AIRCRAFT

摘要

The invention relates to an aircraft including a fuselage and a first measuring probe including means for measuring the local incidence, means for measuring the static pressure, and optionally means for measuring the total pressure. The fuselage includes at least one first zone where the pressure coefficient of the aircraft depends on the unique local incidence irrespective of the sideslip and incidence values of the aircraft, and the first measuring probe is arranged in said first zone

主权项

1. An aircraft comprising:
a fuselage; and a first measuring probe comprising:
an incidence device measuring the local incidence,a pressure device measuring the static pressure, anda total pressure device measuring the total pressure, wherein the fuselage includes at least one first zone where the pressure coefficient of the aircraft depends on the local incidence, which is unique irrespective of the sideslip and incidence values of the aircraft, and wherein the first measuring probe is arranged in said first zone.