FIELD: experimental aerodynamics.
SUBSTANCE: invention relates to the field of experimental aerodynamics, and in particular to methods for determining the aerodynamic characteristics of aircraft. When implementing the method, the characteristics are determined at the current moment, the current environmental conditions, for the current aerodynamic configuration of the aircraft based on the data measured by the hardware on the flight speed during the acceleration of the aircraft in level flight, taking into account the arbitrary setting of the engine thrust vector.
EFFECT: increasing the reliability of determining the main above-mentioned available flight characteristics of the aircraft, taking into account the direction of the engine thrust vector.
1 cl, 1 dwg
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