Aircraft wing structure profiled suspension pylon
According to the invention, the suspension pylon ( 3 ) comprises a fairing for reducing the local loss in lift ( 8 ) and its maximum-width section ( 7 ) is located at the front of the concave and set-back rear part ( 4 R) of the pressure face ( 4 ) of the wing structure ( 1 ). The fairing for reduci...
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| Format: | Patent |
| Sprache: | eng |
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