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Unsteady aerodynamics mitigation for multi-body aerospace apparatus
Unsteady aerodynamics mitigation for multi-body aerospace apparatus
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机译:多体航空航天装置的非定常空气动力学缓解
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摘要
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.
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