AERODYNAMIC HIGH-PERFORMANCE PROFILE FOR AIRCRAFT
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United States of America Patent
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Issued Date -
Jul 30, 2009
app pub date -
Jan 27, 2009
filing date -
Jan 28, 2008
priority date (Note) -
Abandoned
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Abstract
Aerodynamic high-performance profile (10), in which, to force a turbulent flow of the boundary layer away from the bottom side (12), a transition strip (16), which extends over the entire length of the rear edge, is situated in direct proximity to the rear edge (15).
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