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Effect of section thickness and trailing-edge radius on the performance of NACA 65-series compressor blades in cascade at low speeds

机译：截面厚度和后缘半径对低速级联NaCa 65系列压缩机叶片性能的影响

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Herrig, L Joseph; Emery, James C; Erwin, John R;
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年度 1951
页码 1-67
总页数 67
原文格式 PDF
正文语种 eng
中图分类工业技术;
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3. A BLADE DESIGN PERFORMANCE BASED OFF-DESIGN LOSS PREDICTION METHOD FOR AXIAL FLOW COMPRESSORS AND CASCADES [J] . Wu Dongrun, Teng Jinfang, Qiang Xiaoqing, Journal of teoretical and applied mechanics . 2019,第4期

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4. Effects of NACA 65-blade's trailing edge modifications on the performance of a low-speed tube-axial fan [C] . Castegnaro S. Conference of the Italian Thermal Machines Engineering Association . 2016

机译：NACA 65-BLADE后缘改性对低速管轴轴风扇性能的影响
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. Development of a PVDF Sensor Array for Measurement of the Dynamic Pressure Field of the Blade Tip in an Axial Flow Compressor [O] . Jiqing Cong, Jianping Jing, Changmin Chen, 2019

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7. Experimental research on secondary flows in cascade of blades. Effects of blade aspect ratio on the performance of compressor cascade with regard to the Reynolds number effect. [O] . Showgo HAYASHI, Shintaro OTSUKA 1990

机译：叶片级联中次流的实验研究。叶片纵横比对雷诺数效应方面的压缩机级联性能的影响。

Effect of section thickness and trailing-edge radius on the performance of NACA 65-series compressor blades in cascade at low speeds

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