| 火箭发动机小斜切角喷管的设计方法 |
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| 引用本文： | 张铭玉.火箭发动机小斜切角喷管的设计方法[J].推进技术,1989,10(1):14-18,42,72. |
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| 作者姓名： | 张铭玉 |
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| 作者单位： | 新阳机器制造公司 |
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| 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.
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| 关 键 词： | 斜置喷管 推力 火箭发动机 喷管 导弹 |
A METHOD FOR DESIGN OF SMALL BEVEL NOZZLE OF ROCKET ENG INES |
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| Zhang Mingyu.A METHOD FOR DESIGN OF SMALL BEVEL NOZZLE OF ROCKET ENG INES[J].Journal of Propulsion Technology,1989,10(1):14-18,42,72. |
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| Authors: | Zhang Mingyu |
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| Institution: | 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. |
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| Keywords: | Canted nozzle Thrust Approximate calculation Roeket enginenozzle |
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