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PERFORMANCE OF A TRANSONIC COMPRESSOR ROTOR WITH AN ASPECT RATIO OF 6.5

机译：具有6.5的宽高比的跨音压缩机转子的性能

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摘要

This report presents the overall and blade-element performances and the aerodynamic design parameters of a transonic rotor with an aspect ratio of 6. 5, designed to investigate the effects of aspect ratio on range and performance. The rotor was designed for a total-pressure ratio of 1.53, an efficiency of 0.898, and a weight flow of 67.76 pounds per second.

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作者
Lonnie Reid; Edward R. Tysl;
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年度 1974
页码 1-69
总页数 69
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Axial-flow compressor - High aspect ratio - Transonic rotor;

机译：轴流式压缩机 - 高纵横比 - 跨音速转子;

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1. Effect of the specific heat ratio on transonic axial compressor rotor performances [J] . Tian Zhitao, Zheng Qun, Malik Adil, Applied thermal engineering: Design, processes, equipment, economics . 2019,第期

机译：比率对跨音管压缩机转子性能的影响
2. Effect of Partial Span Aspiration on the Performance of a Transonic Axial Compressor Rotor: A Numerical Study [J] . VijaykumarJain, Quamber H.Nagpurwala, AbdulNassar International Journal of Rotating Machinery . 2015,第4期

机译：跨距吸气对跨音速轴流压气机转子性能的影响：数值研究
3. Effect of the Erosion on the Performance of a Transonic Compressor Rotor [J] . Nizar A. Qattan, Ali M. Al-Bahi, Belkacem Kada Journal of Aeronautics Astronautics and Aviation . 2021,第2期

机译：侵蚀对跨音管转子性能的影响
4. NON-AXISYMMETRIC END WALL PROFILING IN TRANSONIC COMPRESSORS. PART II: DESIGN STUDY OF A TRANSONIC COMPRESSOR ROTOR USING NON-AXISYMMETRIC END WALLS - OPTIMIZATION STRATEGIES AND PERFORMANCE [C] . Steffen Raising, Heinz-Peter Schiffer ASME turbo expo . 2009

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5. Numerical Investigation on the Effects of Self-Excited Tip Flow Unsteadiness and Blade Row Interactions on the Performance Predictions of Low Speed and Transonic Compressor Rotors. [D] . Lee, Daniel H. 2013

机译：自激叶尖流动不稳定性和叶片行相互作用对低速和跨音速压缩机转子性能预测影响的数值研究。
6. Hummingbird wing efficacy depends on aspect ratio and compares with helicopter rotors [O] . Jan W. Kruyt, Elsa M. Quicazán-Rubio, GertJan F. van Heijst, 2014

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7. Effect of blade tip winglet on the performance of a highly loaded transonic compressor rotor [O] . Han Shaobing, Zhong Jingjun 2016

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PERFORMANCE OF A TRANSONIC COMPRESSOR ROTOR WITH AN ASPECT RATIO OF 6.5

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