| 发明名称 |
Model blade for flow simulation has chord length and surface of subsonic model blade scaled to simulate supersonic flow |
| 摘要 |
<p>The model blade is to simulate the flow of the transonic flow relation of a gas turbine blade in a compressor by means of subsonic flow over the model blade. The chord length and the surface of the model blade which is to be subjected to the subsonic flow are scaled in such a manner as to simulate the transonic flow relation of the gas turbine blade being simulated.</p> |
| 申请公布号 |
DE102004046128(A1) |
申请公布日期 |
2006.04.06 |
| 申请号 |
DE20041046128 |
申请日期 |
2004.09.23 |
| 申请人 |
MTU AERO ENGINES GMBH |
发明人 |
BAIER, RALF-DIETMAR;ENGEL, KARL;HOEGER, MARTIN;KRAUS, JUERGEN |
| 分类号 |
F15D1/10 |
主分类号 |
F15D1/10 |
| 代理机构 |
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