Device to reduce the lateral force generated by an aerial refueling boom (11) of an aircraft characterized in that it has at least one plate (31), the plate (31) has two cantilevered wings (32, 33), the wings (32, 33) have perforations (34), so that the wake produced in the boom (11) has a lower dynamic pressure than that of the free stream.

 
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< Luggage compartment that can be lowered comprising a hydraulic cylinder locking mechanism

< Flight passenger seat with an integrated spring element

> High-performance low-noise aircraft exhaust systems and methods

> Systems and methods for providing differential motion to wing high lift device

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