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Experimental determination of aerodynamic forces normal to the chord due to rotating stall acting on compressor blading

机译：由于旋转失速作用于压缩机叶片而实际确定与弦杆垂直的气动力

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Johnson, Donald F; Costilow, Eleanor L;
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年度 1954
页码 1-30
总页数 30
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Numerical Study on Stall Flutter of A Compressor Cascade (2nd Report, Relationship between Unsteady Aerodynamic Characteristics of Oscillating Blades and Rotating Stall) [J] . Toshio NISHIZAWA, Hiroyuki TAKATA 日本機械学会論文集. B編 . 1999,第635期

机译：压缩机叶栅失速颤振的数值研究（第二份报告，动叶片非定常空气动力特性与旋转失速之间的关系）
2. Unsteady Aerodynamic Blade Excitation at the Stability Limit and During Rotating Stall in an Axial Compressor [J] . Ronald Mailach, Konrad Vogeler Journal of turbomachinery . 2007,第3期

机译：轴流压气机在稳定极限和旋转失速期间的非稳态气动叶片激励
3. A Systematic Approach to Estimate the Impact of the Aerodynamic Force Induced by Rotating Stall in a Vaneless Diffuser on the Rotordynamic Behavior of Centrifugal Compressors [J] . Alessandro Bianchini, Davide Biliotti, Giovanni Ferrara, Journal of Engineering for Gas Turbines and Power . 2013,第11期

机译：一种估计无叶片扩压器中的旋转失速所产生的空气动力对离心压缩机的旋转动力学行为影响的系统方法
4. NUMERICAL IDENTIFICATION OF LOW-FREQUENCY HARMONICS OF FORCES ACTING ON HPC ROTOR BLADES DUE TO ROTATING STALLS [C] . Vladimir Makarov, Victor Shorstov, Sergej Andreev, International Symposium on Air Breathing Engines . 2017

机译：由旋转旋转旋转旋转叶片作用于HPC转子叶片的低频谐波的数值识别
5. An analytical and experimental investigation of the active control of rotating stall in a low speed centrifugal compressor. [D] . Lawless, Patrick Benjamin. 1993

机译：低速离心压缩机旋转失速主动控制的分析和实验研究。
6. Rotating Stall Induced Non-Synchronous Blade Vibration Analysis for an Unshrouded Industrial Centrifugal Compressor [O] . Xinwei Zhao, Qiang Zhou, Shuhua Yang, 2019

机译：无罩工业离心压缩机的旋转失速诱导非同步叶片振动分析
7. Numerical Study on Stall Flutter of a Compressor Cascade. (2nd Report, Relationship between Unsteady Aerodynamic Characteristics of Oscillating Blades and Rotating Stall). [O] . Toshio NISHIZAWA, Hiroyuki TAKATA 2000

机译：压缩机级联失速颤动的数值研究。（第2次报告，不稳定空气动力学特性的振动叶片和旋转旋转的关系）。

Experimental determination of aerodynamic forces normal to the chord due to rotating stall acting on compressor blading

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