|
|||||
|
|
| 跨声速多级轴流压气机非设计性能预测 | |
| 引用本文： | 杜文海,吴虎,黄健. 跨声速多级轴流压气机非设计性能预测[J]. 航空动力学报, 2007, 22(9): 1481-1486 |
| 作者姓名： | 杜文海 吴虎 黄健 |
| 作者单位： | 西北工业大学,动力与能源学院,西安,710072;西北工业大学,动力与能源学院,西安,710072;西北工业大学,动力与能源学院,西安,710072 |
| 摘 要： | 基于公开发表的研究成果, 发展了一种适用于跨声速轴流压气机的新型损失和落后角模型, 并进行了3-D的修正, 运用改进的流线曲率法对某两级跨声速轴流压气机进行了数值模拟, 得到了设计点和非设计点的特性曲线.通过计算结果与实验值的比较, 验证了本模型和方法在设计点和非设计点均具较高的精度, 可用于工程计算. |
| 关 键 词： | 航空、航天推进系统 流线曲率法 跨声速 轴流压气机 非设计 损失落后角模型 |
| 文章编号： | 1000-8055(2007)09-1481-06 |
| 收稿时间： | 2006-08-24 |
| 修稿时间： | 2006-08-24 |
Off-design performance prediction of multi-stage transonic axial compressor |
|
| DU Wen-hai,WU Hu and HUANG Jian. Off-design performance prediction of multi-stage transonic axial compressor[J]. Journal of Aerospace Power, 2007, 22(9): 1481-1486 | |
| Authors: | DU Wen-hai WU Hu HUANG Jian |
| Affiliation: | School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China |
| Abstract: | A new loss and deviation model suitable for multi-stage transonic axial compressor was developed according to the research findings publicly available.Along with 3-D modification,numerical simulation was performed for two-stage transonic axial compressor using an improved streamline curvature method,thus obtaining the characteristic curve of design point and off-design point.By combining the calculated results with experimental value,this model and method are suitable for engineering calculation with higher accuracy of design point and off-design point. |
| Keywords: | aerospace propulsion system streamline curvature transonic axial compressor off-design loss and deviation model |
| 本文献已被 CNKI 万方数据 等数据库收录！ | |
| 点击此处可从《航空动力学报》浏览原始摘要信息 | |
| 点击此处可从《航空动力学报》下载全文 | |