首页> 美国政府科技报告 >Design and investigation of a transonic axial-flow compressor rotor with an inlet hub-tip radius ratio of essentially zero

【24h】

Design and investigation of a transonic axial-flow compressor rotor with an inlet hub-tip radius ratio of essentially zero

机译：跨音速轴流式压缩机转子的设计和研究，入口轮毂半径比基本为零

获取原文

页面导航

摘要
著录项
引文网络
相似文献
相关主题

摘要

No Abstract Available

著录项

作者
Westphal, Willard R; Maynard, John W , Jr;
展开▼
作者单位

展开▼
年度 1957
页码 1-38
总页数 38
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词

相似文献

外文文献
中文文献
专利

1. Modelling of turbulent flows in transonic axial-flow compressor NASA Rotor 37 with local weak-equilibrium damping of eddy viscosity coefficient [J] . A.N. Aksyonov, A.B. Shabarov Thermophysics and Aeromechanics . 2009,第4期

机译：跨音速轴流压气机NASA转子37中湍流的局部涡流系数弱平衡建模
2. Numerical simulation of transonic compressor under circumferential inlet distortion and rotor/stator interference using harmonic balance method [J] . Wang Ziwei, Jiang Xiong, Chen Ti, Modern Physics Letters, B. Condensed Matter Physics, Statistical Physics, Applied Physics . 2018,第12a13期

机译：谐波平衡法在圆周入口失真与转子/定子干扰下跨音速压缩机的数值模拟
3. Non-uniform stator loss reduction design strategy in a transonic axial-flow compressor stage under inflow distortion [J] . Lu Hanan, Yang Zhe, Pan Tianyu, Aerospace science and technology . 2019,第SEPa期

机译：跨音速轴流压气机工况下定子涡流非均匀性降低的设计策略
4. AN EXPERIMENTAL INVESTIGATION ABOUT THE EFFECT OF THE PARTIAL CASING TREATMENT ON A TRANSONIC AXIAL-FLOW COMPRESSOR PERFORMANCE UNDER INLET DISTORTION [C] . Maoyi Li, Wei Yuan, Xizhen Song, ASME turbo expo . 2012

机译：进气畸变下部分套管处理对跨音速轴流压气机性能影响的实验研究
5. Stepped tip gap effects on a transonic axial-flow compressor rotor [D] . Thompson, Donald William 1997

机译：阶梯间隙对跨音速轴流压缩机转子的影响
6. A Vibration Sensor-Based Method for Generating the Precise Rotor Orbit Shape with General Notch Filter Method for New Rotor Seal Design Testing and Diagnostics [O] . Karel Kalista, Jindrich Liska, Jan Jakl 2021

机译：一种基于振动传感器的方法用于产生精确的转子轨道形状具有新的转子密封设计测试和诊断的一般陷波滤波器方法
7. Experimental Vibration Damping Characteristics of the Third-stage Rotor of a Three-stage Transonic Axial-flow Compressor [O] . Newman Frederick A. 1988

机译：三级跨音速轴流压缩机三级转子的实验减振特性

Design and investigation of a transonic axial-flow compressor rotor with an inlet hub-tip radius ratio of essentially zero

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅