首页> 外文OA文献 >Studies on the Limits of Surging in Multi-Stage Axial-Flow Compressor : 1st Report, Methods for Calculating the Surging Points

【2h】

Studies on the Limits of Surging in Multi-Stage Axial-Flow Compressor : 1st Report, Methods for Calculating the Surging Points

机译：多级轴流压缩机澎湃的限制：第1报告，计算浪涌点的方法

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
Kazuo TAKEYA;
展开▼
作者单位

展开▼
年度 1961
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. A Study on the Fundamental Surge Frequencies in Multi-Stage Axial Flow Compressor Systems [J] . Nobuyuki Yamaguchi International Journal of Fluid Machinery and Systems . 2014,第4期

机译：多级轴流压气机系统基本喘振频率的研究
2. Influence Of Inlet Parameters On Centrifugal Compressor Surge Limit Line: Case study uses numerical analysis to examine effects of variations [J] . MASSIMILIANO DI FEBO, PASQUALE PAGANINI CompressorTech Two: Dedicated to Gas Compression Products and Applications . 2013,第5期

机译：进气口参数对离心压缩机喘振极限线的影响：案例研究使用数值分析来检查变化的影响
3. Numerical Study on Stall Flutter of A Compressor Cascade (1st Report, Numerical Method and Numerical Example) [J] . Toshio NISHIZAWA, Hiroyuki TAKATA 日本機械学会論文集. B編 . 1999,第635期

机译：压缩机叶栅失速颤动的数值研究（第一报告，数值方法和数值示例）
4. Numerical simulations of surge and rotatil stall in multi-stage axial-flow compressor [C] . J.F.Escuret, V.Garnier 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference June 27-29, 1994/Indianapolis, IN . 1994

机译：多级轴流压缩机喘振和旋转失速的数值模拟
5. Flow Characterization and Dynamic Analysis of a Radial Compressor with Passive Method of Surge Control [D] . Guillou, Erwann 2011

机译：被动控制喘振方法的径向压缩机流动特性及动力学分析
6. Generation Mechanisms of Rotating Stall and Surge in Centrifugal Compressors [O] . Elias Sundström, Bernhard Semlitsch, Mihai Mihăescu -1

机译：离心压缩机旋转失速和喘振的产生机理
7. Studies on the Limits of Surging in Multi-Stage Axial-Flow Compressor : 2nd Report, Consideration Concerning the Surging Characteristics [O] . Kazuo TAKEYA 1961

机译：多级轴流压缩机澎湃的限制：第2次报告，思考飙升特征
8. Effect of rotor-and stator-blade modifications on surge performance of an 11-stage axial-flow compressor I : original production compressor of XJ40-WE-6 engine [R] . Finger, Harold B, Essig, Robert H, Conrad, E William 1953

机译：转子和定子叶片改造对11级轴流式压缩机喘振性能的影响I：XJ40-WE-6发动机的原始生产压缩机

Studies on the Limits of Surging in Multi-Stage Axial-Flow Compressor : 1st Report, Methods for Calculating the Surging Points

著录项

引文网络

相似文献

相关主题

期刊订阅