摘要
To address the issue of low cooling efficiency at the crests of longitudinally corrugated heat shields, a novel structural—a non-uniformly distributed longitudinally corrugated heat shield with inclined perforations only on the leeward side of the troughs, was proposed. Using commercial CFD software and fluid-solid coupled numerical simulation methods,comparative studies were conducted with traditional structural schemes including uniformly distributed and graded-density configurations. The cooling performance of the heat shield's wall was analyzed under hole inclination angles ranging from 20° to 40° and blowing ratios between 0.82 and 1.85,and the effects of inclination angle and blowing ratio on cooling efficiency were examined. The results showed that the proposed design effectively utilized dynamic pressure intake on the leeward side, significantly reduced high-temperature zones on the wall,improved crest cooling efficiency,and enhanced wall temperature uniformity. A smaller inclination angle decreased trough cooling efficiency but increased crest cooling efficiency,with the crest cooling efficiency reaching its peak at an inclination angle of 30° to 35°,representing a 5.62% improvement compared with the baseline model. At a blowing ratio of 1.85, the maximum enhancement in crest cooling efficiency reached 5.57% compared with the baseline model,though accompanied by a 7.57% reduction in cooling efficiency uniformity coefficient.
| 投稿的翻译标题 | Study on film cooling characteristics of non-uniform layout corrugated heat shield with inclined holes on leeward side |
|---|---|
| 源语言 | 繁体中文 |
| 期刊论文编号 | 20250011 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 41 |
| 期 | 7 |
| DOI | |
| 出版状态 | 已出版 - 7月 2026 |
关键词
- afterburner
- blowing ratio
- film cooling
- hole inclination angle
- longitudinal corrugated heat shield
学术指纹
探究 '背风侧倾斜开孔的非均匀布局波纹隔热屏气膜冷却特性研究' 的科研主题。它们共同构成独一无二的学术指纹。引用此
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