发明名称 |
Dynamic bumps for drag reduction at transonic-supersonic speeds |
摘要 |
A system for reducing overall drag of a mobile platform includes a surface on which an airflow forms a boundary layer and a generally normal shockwave. The airflow is at a first velocity that is one of transonic and supersonic. An oscillating jet injects and extracts a jet flow through the surface. The jet flow is at a second velocity that is substantially less than the first velocity. A recirculation region is upstream of the normal shockwave and is disposed at least partially in the boundary layer. The recirculation region is established at least by the oscillating jet. A generally oblique wave is established by the recirculation region and weakens the normal shockwave to reduce the overall drag experienced by the surface.
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申请公布号 |
US8016245(B2) |
申请公布日期 |
2011.09.13 |
申请号 |
US20060583140 |
申请日期 |
2006.10.18 |
申请人 |
THE BOEING COMPANY |
发明人 |
HASSAN AHMED A.;OSBORNE BRADLEY A.;SCHWIMLEY SCOTT;BILLMAN GARRY |
分类号 |
B64C21/08;B64C23/04;B64C23/06 |
主分类号 |
B64C21/08 |
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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