发明名称 |
Process to minimize turbine airfoil downstream shock induced flowfield disturbance |
摘要 |
A process of designing a transonic airfoil that results in an exit deviation angle that is optimized to minimize downstream shock induced flowfield disturbances. Specifically, a design process of a transonic airfoil minimizes pitchwise variation in downstream static pressure that includes determining an airfoil exit deviation angle and downstream turning for reduced shock from a trailing edge of the transonic airfoil.
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申请公布号 |
US2007033802(A1) |
申请公布日期 |
2007.02.15 |
申请号 |
US20050204261 |
申请日期 |
2005.08.09 |
申请人 |
HONEYWELL INTERNATIONAL, INC. |
发明人 |
MCKEEVER CRAIG W. |
分类号 |
B21D53/78 |
主分类号 |
B21D53/78 |
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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