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.
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
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