首页> 外文会议>AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit >Influence of Tip Clearance Size on Flow Characteristics of a Vaneless Counter- Rotating Turbine

【24h】

Influence of Tip Clearance Size on Flow Characteristics of a Vaneless Counter- Rotating Turbine

机译：叶尖间隙尺寸对无叶片反向旋转涡轮机流动特性的影响

获取原文

页面导航

著录项
相似文献
相关主题

著录项

来源
《AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit》|2009年|P.1-14|共14页
会议地点
作者
Q. Zhao; J. Qiao; H. Wang; X. Zhao; J. Xu;
展开▼
作者单位

展开▼
会议组织
原文格式 PDF
正文语种
中图分类航空发动机（推进系统）;推进系统（发动机、推进器）;
关键词

相似文献

外文文献
中文文献
专利

1. Tip Clearance Effects on Inlet Hot Streak Migration Characteristics in High Pressure Stage of a Vaneless Counter-Rotating Turbine [J] . Zhao Qingjun, Du Jianyi, Wang Huishe, Journal of turbomachinery . 2010,第1期

机译：叶片间隙对无叶片反向旋转涡轮高压阶段进气热条纹迁移特性的影响
2. Investigation on tip clearance control for the high-pressure rotor of an uncooled vaneless counter-rotating turbine [J] . Wei Zhao, Xiuming Sui, Kai Zhang, Proceedings of the Institution of Mechanical Engineers . 2021,第5期

机译：一种未冷却差旋转旋转涡轮机高压转子尖端间隙的研究
3. Tip-Clearance Effects on Hot-Streak Migration in Low-Pressure Stage of Vaneless Counter-Rotating Turbine [J] . Qingjun Zhao, Huishe Wang, Xiaolu Zhao, Journal of propulsion and power . 2009,第4期

机译：无叶片反向旋转涡轮低压阶段的尖部间隙对热条纹迁移的影响
4. Influence of Tip Clearance Size on Flow Characteristics of a Vaneless Counter- Rotating Turbine [C] . Q. Zhao, J. Qiao, H. Wang, AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2009

机译：尖端间隙尺寸对无差旋转涡轮机的流动特性的影响
5. Comparison of Traditional Two-spool and Three-spool with Vaneless Counter-rotating Low-pressure Turbine for Aircraft Propulsion Power Extraction [D] . Burgett, Luke Michael 2019

机译：传统两阀芯和三阀芯无叶片反向旋转低压涡轮机用于飞机推进力提取的比较
6. Investigation of the Pressure Gain Characteristics and Cycle Performance in Gas Turbines Based on Interstage Bleeding Rotating Detonation Combustion [O] . Lei Qi, Zhitao Wang, Ningbo Zhao, 2019

机译：基于间隙旋转爆轰燃烧的燃气轮机压力增益特性及循环性能研究
7. On the Characteristics of Wing with Tip Clearance : 1st Report, The Influences of the Wing-Tip Clearance Contained within a Non-Uniform Flow [O] . Shintaro OTSUKA, Yoshiyuki SUGIYAMA, Hisao MUROI, 1966

机译：关于尖端间隙的机翼特征：第1报告，翼尖间隙的影响不均匀

获取原文

客服邮箱：kefu@zhangqiaokeyan.com

京公网安备：11010802029741号 ICP备案号：京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有

客服微信
服务号