发明名称 |
Loss reduction device for compression shock includes at least one shock-inducing body spaced out from surface in supersonic flow region |
摘要 |
The loss reduction device reduces the compression shock (7) in the supersonic flow region (6) of a surface (5). A shock-inducing device (10) induces a weak shock in the flow, causing at least a 20% reduction in the cross section of the flow passing through the supersonic flow region. At least one shock-inducing device, consisting of a body (9), is spaced out from the surface in the supersonic flow region.
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申请公布号 |
DE10305973(B3) |
申请公布日期 |
2004.05.06 |
申请号 |
DE2003105973 |
申请日期 |
2003.02.13 |
申请人 |
DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V. |
发明人 |
REIN, MARTIN;ROSEMANN, HENNING;SCHUELEIN, ERICH |
分类号 |
B64C3/00;B64C3/14;B64C21/00;B64C23/00;(IPC1-7):B64C21/00 |
主分类号 |
B64C3/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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