| F/A-18E/F飞机发动机的CARET进气道 |
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| 引用本文： | 杨国才.F/A-18E/F飞机发动机的CARET进气道[J].推进技术,1997,18(4):31-35. |
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| 作者姓名： | 杨国才 |
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| 作者单位： | 成都飞机设计研究所!成都，610041 |
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| 摘 要： | 介绍了与F／A－18E／F飞机发动机提高性能相适应的、设计Ma=2．0的固定几何的“CARET”进气道的设计，分析了新设计的E／F进气道性能和机体／进气道一体化的模型风洞试验结果。该进气道新概念设计对我国在研或预研的某些机种都有较好的参考与借鉴价值。
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| 关 键 词： | 飞机发动机 进气道 设计 |
THE CARET INLET OF THE F/A-18E/F STRIKE FIGHTER |
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| Yang Guocai.THE CARET INLET OF THE F/A-18E/F STRIKE FIGHTER[J].Journal of Propulsion Technology,1997,18(4):31-35. |
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| Authors: | Yang Guocai |
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| Affiliation: | Chengdu Aircraft Design &. Research Inst., Chengdu, 610041 |
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| Abstract: | A new fixed geometric Mach 2. 0"CARET"inlet was introduced and analyzed. A wind tunnel development program has been successfully completed, utilizing both isolated inlet and full integrated inlet/airframe models. The new F/A-18E/F inlet represents a balanced design for aircraft performace, maneuvering and producibility. The first flight of "E"type was succeed in December 1995. |
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| Keywords: | Airplane engine Inlet Design |
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