| 摘要: |
| 根据火箭发动机的推力公式及空气动力学有关理论,导出在小斜切角喷管内气体流动的特性、推力的变化规律,并给出喷管的设计方法. |
| 关键词: 斜置喷管 推力 近似计算 火箭发动机喷管 |
| DOI： |
| 分类号: |
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| A METHOD FOR DESIGN OF SMALL BEVEL NOZZLE OF ROCKET ENG INES |
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Zhang Mingyu
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Zhang Mingyu (Xinyang Machinery Manufacture Co.
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| Abstract: |
| In this paper, the aerodynamic performance and the thrust performance of the small bevel nozzle of rocket engines are developed based on thrust equation of rocket engines and theories in aerodynamics. A design method of this kind of nozzles is also presented. |
| Key words: Canted nozzle Thrust Approximate calculation Roeket enginenozzle |
