The invention relates to a flow body (10) for an aircraft (100). The flow body (10) comprises a recess (12) in a surface (16) of the flow body (10), a first structural component (21) with a porous material and may also comprise a second structural component (22) with a porous material. The recess (12) comprises a front recess region (31) and a rear recess region (32). The first structural component (21) is arranged in, or on, the front recess region (31) and the second structural component (22) may be arranged in, or on, the rear recess region (32). The invention further relates to an aircraft (101) having the flow body (10), a weapons system (110) having the flow body (10) and a method for manufacturing a flow body (10) for a vehicle (100).
FLOW BODY FOR A VEHICLE AND METHOD FOR MANUFACTURING A FLOW BODY
STRÖMUNGSKÖRPER FÜR EIN FAHRZEUG UND VERFAHREN ZUR HERSTELLUNG EINES STRÖMUNGSKÖRPERS
CORPS D'ÉCOULEMENT POUR UN VÉHICULE ET PROCÉDÉ DE FABRICATION D'UN CORPS D'ÉCOULEMENT
2022-05-04
Patent
Elektronische Ressource
Englisch
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