| 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。 |
| 关键词: 飞机发动机 进气道 设计 |
| DOI： |
| 分类号:V23 |
| 基金项目: |
|
| THE CARET INLET OF THE F/A-18E/F STRIKE FIGHTER |
|
Yang Guocai
|
|
Chengdu Aircraft Design &. Research Inst., Chengdu, 610041
|
| 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. |
| Key words: Airplane engine Inlet Design |
