A multi-body aerospace apparatus includes a first aerospace body (12), a second aerospace body (14), and a flow separation member (18). The second aerospace body is attached adjacent to the first aerospace body with a gap (20) disposed between the first aerospace body and the second aerospace body. The flow separation member is attached to the first aerospace body or to the second aerospace body.
Unsteady aerodynamics mitigation for multi-body aerospace apparatus
Minderung instationärer Aerodynamik für Mehrkörper-Raumfahrvorrichtung
Atténuation d'aérodynamisme non stationnaire pour appareil aérospatial multicorps
2020-09-30
Patent
Electronic Resource
English
Unsteady Aerodynamics of a Rapidly Tumbling Bluff Body
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