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
Aéronef comprenant une sonde de mesure et procédé de détermination de paramètres de vol d'un tel aéronef
Aircraft including a measuring probe and method for determining flight parameters of such an aircraft
Luftfahrzeug, das eine Messsonde umfasst, und Verfahren zur Bestimmung der Flugparameter eines solchen Luftfahrzeugs
2017-08-09
Patent
Electronic Resource
French
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