| 摘要 |
An aircraft wing 10 includes a blister 14 for either housing at least a part of one or more sensors (e.g. air pressure sensors), or having at least a part of one or more sensors mounted to or integrated with an outer surface of the blister 14. The blister 14 is positioned on an underside portion of the aircraft wing 10 such that the blister 14 does not project from the underside of the aircraft wing 10 beyond a leading edge 12 of the aircraft wing 10 in a direction parallel to a roll axis of the aircraft 2. In addition, the blister 14 does not project from the underside of the aircraft wing 10 beyond a lowermost surface of the aircraft wing 10 in a direction parallel to a yaw axis of the aircraft 2.
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