发明名称 |
ROCKET ENGINE NOZZLE |
摘要 |
The invention refers to a rocket engine nozzle with an outlet portion having a curved profile in axial section. In order to enable a control of the flow separation occurring within the nozzle outlet, it is suggested that, circumferentially, said outlet portion in axial section has a radius, the length of which varies.
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申请公布号 |
WO9729277(A1) |
申请公布日期 |
1997.08.14 |
申请号 |
WO1996SE00176 |
申请日期 |
1996.02.12 |
申请人 |
VOLVO AERO CORPORATION;HAEGGANDER, JAN;PEKKARI, LARS-OLOF |
发明人 |
HAEGGANDER, JAN;PEKKARI, LARS-OLOF |
分类号 |
F02K9/97;(IPC1-7):F02K9/97 |
主分类号 |
F02K9/97 |
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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