| 摘要: |
| 详细介绍了弹用航空发动机红外抑制技术开展的一系列试验和数值分析。这些工作均取得了较好的结果，为今后此项技术的进一步深入研究直至工程应用打下了良好的基础。 |
| 关键词: 航空发动机 喷管气流 红外特征 红外抑制 |
| DOI： |
| 分类号:V231.3 |
| 基金项目: |
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| A RESEARCH ON RADIATION RESTRICTION TECHNIQUE OF A NOZZLE FLOW OF AERO-ENGINE FOR MISSILE |
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Beijing Electro-Mechanical Engineering Inst., Beijing, 100074
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| Abstract: |
| In this paper experiments and the numerical analyses about infrared restriction technique of aero-engine is described in detail. Satisfactory results are obtained, which lay a good functionfor the future research and application. |
| Key words: Aircraft engine Nozzle gas flow Infrared signature Infrared suppression |
