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Investigation of a 10-stage subsonic axial-flow research compressor V : effect of reducing inlet-guide-vane turning on over-all and inlet-stage performance

机译：对10级亚音速轴流研究压缩机的研究V：减少进气导叶转向对整体和进气级性能的影响

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Budinger, Ray E; Serovy, George K;
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年度 1954
页码 1-39
总页数 39
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Numerical Investigation Of Tandem Airfoils For Subsonic Axial-flow Compressor Blades [J] . Jonathan McGlumphy, Winq-Fai Ng, Steven R. Wellborn, Journal of turbomachinery . 2009,第2期

机译：亚音速轴流压气机叶片串联翼型的数值研究
2. Numerical and Experimental Investigations of Steady Micro-Tip Injection on a Subsonic Axial-Flow Compressor Rotor [J] . Xingen Lu, Wuli Chu, Junqiang Zhu, International Journal of Rotating Machinery . 2006,第0期

机译：亚音速轴流压气机转子上稳定微尖喷射的数值和实验研究
3. Numerical and Experimental Investigations of Steady Micro-Tip Injection on a Subsonic Axial-Flow Compressor Rotor [J] . XingenLu, WuliChu, JunqiangZhu, International Journal of Rotating Machinery . 2006,第2期

机译：亚音速轴流压气机转子上稳定微尖喷射的数值和实验研究
4. NUMERICAL INVESTIGATION OF TANDEM AIRFOILS FOR SUBSONIC AXIAL-FLOW COMPRESSOR BLADES [C] . Jonathan McGlumphy, Wing-Fai Ng, Steven R. Wellborn, IMECE2007;ASME International Mechanical Engineering Congress and Exposition;American Society of Mechanical Engineers International Mechanical Engineering Congress and Exposition(IMECE2007) . 2008

机译：亚音速轴流压气机叶片的串联翼型的数值研究
5. A METHOD FOR THE PREDICTION OF THE OFF-DESIGN PERFORMANCE OF AXIAL-FLOW COMPRESSORS. [D] . SEROVY, GEORGE KASPAR. 1958

机译：一种预测轴流式压缩机偏离性能的方法。
6. Investigating the performance and cost-effectiveness of the simple ultrasound-based rules compared to the risk of malignancy index in the diagnosis of ovarian cancer (SUBSONiC-study): protocol of a prospective multicenter cohort study in the Netherlands [O] . Evelyne MJ Meys, Iris JG Rutten, Roy FPM Kruitwagen, 2015

机译：在卵巢癌的诊断中研究基于简单超声的规则与恶性指数风险相比的性能和成本效益（SUBSONiC研究）：荷兰一项前瞻性多中心队列研究的方案
7. Stage effects on stalling and recovery of a high-speed 10-stage axial-flow compressor [O] . Copenhaver, William Ward 1988

机译：高速10级轴流式压缩机失速和恢复的阶段效应

Investigation of a 10-stage subsonic axial-flow research compressor V : effect of reducing inlet-guide-vane turning on over-all and inlet-stage performance

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