A flow body for an aircraft includes a recess in a surface of the flow body, a first structural component with a porous material and may also include a second structural component with a porous material. The recess includes a front recess region and a rear recess region. The first structural component is arranged in, or on, the front recess region and the second structural component may be arranged in, or on, the rear recess region. An aircraft having the flow body, a weapons system having the flow body and a method for manufacturing a flow body for a vehicle are also described.
Flow Body For A Vehicle And Method For Manufacturing A Flow Body
2022-07-07
Patent
Elektronische Ressource
Englisch
FLOW BODY FOR A VEHICLE AND METHOD FOR MANUFACTURING A FLOW BODY
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