摘要
To develop a rapid and efficient method for contour design of linear plug nozzle, the obliquity of internal nozzle and the expansion ratios of plug nozzle and internal nozzle, which were related to the expansion capability, were theoretically analyzed. Two second-degree polynomials and a third-degree polynomial were adopt to describe the contours of a linear plug nozzle, and the means in determining nozzle contours were also presented. The influence of the plug nozzle expansion ratios on its figure dimensions was studied. Two types of plug nozzles designed by the rapid method were tested with cold flow. The experimental results demonstrate the excellent altitude compensating capability.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 144-147+169 |
| 期刊 | Tuijin Jishu/Journal of Propulsion Technology |
| 卷 | 25 |
| 期 | 2 |
| 出版状态 | 已出版 - 4月 2004 |
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