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AIRCRAFT AERODYNAMIC PROFILE ON OPEN ATTACK, MAT AND AIRCRAFT HAVING SUCH AERODYNAMIC PROFILE
AIRCRAFT AERODYNAMIC PROFILE ON OPEN ATTACK, MAT AND AIRCRAFT HAVING SUCH AERODYNAMIC PROFILE
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机译:飞机有气动特性时,飞机在空袭,垫子和飞机上的气动特性
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摘要
The invention relates to an aerodynamic aircraft profile comprising a profile (1) constituting a leading edge (BA) of the aerodynamic profile. The profile (1) comprises an opening at said leading edge (BA) allowing the entry of air into the thickness of said aerodynamic profile, an air outlet, and shaped guiding means for guiding the air towards the air outlet. The opening at the leading edge makes it possible to introduce air into the thickness of the profile, limiting the aerodynamic turbulence at said leading edge. The invention also relates to a mast carrying an aircraft propulsion unit and having such an aerodynamic profile. The invention finally relates to an aircraft equipped with such a profile.
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