首页> 外文OA文献 >Multi-Objective Optimization of Three-Dimensional Blade Shape for an Axial Compressor Rotor in Transonic Stage

【2h】

Multi-Objective Optimization of Three-Dimensional Blade Shape for an Axial Compressor Rotor in Transonic Stage

机译：跨音级轴向压缩机转子的三维叶片形状的多目标优化

代理获取

本网站仅为用户提供外文OA文献查询和代理获取服务，本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文，但由于OA文献来源多样且变更频繁，仍可能出现获取不到、文献不完整或与标题不符等情况，如果获取不到我们将提供退款服务。请知悉。

页面导航

著录项
引文网络
相似文献
相关主题

著录项

作者
Chihiro Myoren; Yasuo Takahashi; Yasuhiro Kato;
展开▼
作者单位

展开▼
年度 2013
总页数
原文格式 PDF
正文语种
中图分类

相似文献

外文文献
中文文献
专利

1. Optimization of Blade Sweep in a Transonic Axial Compressor Rotor [J] . Choon-Man JANG, Ping LI, Kwang-Yong KIM JSME International Journal. Series B, Fluids and Thermal Engineering . 2005,第4期

机译：跨音速轴向压气机转子叶片扫掠的优化
2. Three-Dimensional Design and Optimization of a Transonic Rotor in Axial Flow Compressors [J] . Hidetaka Okui, Tom Verstraete, R. A. Van den Braembussche, Journal of turbomachinery . 2013,第3期

机译：轴流压气机跨音速转子的三维设计与优化
3. Shape optimization of an axial compressor blade by multi-objective genetic algorithm [J] . A Samad K-Y Kim Proceedings of the Institution of Mechanical Engineers . 2008,第A6期

机译：基于多目标遗传算法的轴流压气机叶片形状优化
4. Optimization of rotor blade in stage circumstance for transonic axial flow compressor [C] . Jinxin Cheng, Jiang Chen, Hang Xiang IEEE Conference on Industrial Electronics and Applications . 2017

机译：跨音速轴流压气机分级工作时转子叶片的优化
5. Influence of axial spacing on spanwise efficiency of a transonic axial compressor rotor stage. [D] . Davey, Mark Willis. 2004

机译：轴向间距对跨音速轴向压缩机转子级的翼展方向效率的影响。
6. Non-Contact Measurement of Blade Vibration in an Axial Compressor [O] . Radoslaw Przysowa, Peter Russhard 2020

机译：轴流压缩机中叶片振动的非接触式测量
7. Large scale optimization of transonic axial compressor rotor blades [O] . Shahpar S., Polynkin A., Toropov V. 2008

机译：跨音速轴流压气机转子叶片的大规模优化
8. Experimental investigation of an axial-flow compressor inlet stage operating at transonic relative inlet Mach numbers III : blade-row performance of stage with transonic rotor and subsonic stator at corrected tip speeds of 800 and 1000 feet per secon [R] . Schwenk, Francis C, Lieblein, Seymour, Lewis, George W , Jr 1953

机译：在跨音速相对入口处操作的轴流式压缩机入口级的实验研究马赫数III：具有跨音速转子和亚音速定子的级的叶片排性能，校正的尖端速度为800和1000英尺/秒

Multi-Objective Optimization of Three-Dimensional Blade Shape for an Axial Compressor Rotor in Transonic Stage

著录项

引文网络

相似文献

相关主题

期刊订阅