Device for Generating Aerodynamic Resistance on an Aircraft
An aircraft (1) has a brake flap (6) arranged upstream of a vertical tail (4), which brake flap (6) can be pivoted out into the air flow approaching the vertical tail (4). To reduce dynamic structural loading of the vertical tail (4), through openings (7, 8) are formed in the brake flap (6).
BREITSAMTER CHRISTIAN [DE]
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