| 大函道比涡扇发动机试车台气动力设计的特点 |
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| 引用本文： | 国绍荣.大函道比涡扇发动机试车台气动力设计的特点[J].航空学报,1987,6(6):251-255. |
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| 作者姓名： | 国绍荣 |
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| 作者单位： | 航空工业部第四规划设计研究院 |
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| 摘 要： | 本文简要地阐述了大函道比涡扇发动机试车间气动设计的特点;并结合民航7907试车台的建设经验,讨论了保持试车间流场均匀的极端重要性。这些经验对于我们今后设计大函道比涡扇发动机和螺浆风扇发动机试车台时,将是十分有用的。
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| 收稿时间： | 1986-07-10; |
AERODYNAMIC DESIGN CHARACTERISTIC OF TEST CELL FOR-HIGH. BY-PASS RATIO TURBOFAN ENGINE |
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| Guo Shaorong.AERODYNAMIC DESIGN CHARACTERISTIC OF TEST CELL FOR-HIGH. BY-PASS RATIO TURBOFAN ENGINE[J].Acta Aeronautica et Astronautica Sinica,1987,6(6):251-255. |
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| Authors: | Guo Shaorong |
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| Institution: | China Aeronautical Project and Design Institute |
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| Abstract: | This article briefly introduced the aerodynamic design characteristic of test cell for high by-pass ratio turbofan engine and discussed the extreme importance of keeping an uniform flow distribution in the test cell with the consideration of the construction experience of 7907 test cell for CAAC.This experience will be very helpful in the design of test for high by-pass ratio turbofan engine and propeller-fan engine. |
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