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ALTITUDE-WIND-TUNNEL INVESTIGATION OF A 4000-POUND-THRUST AXIAL-FLOW TURBOJET ENGINEⅢ- PERFORMANCE CHARACTERISTICS WITH THE HIGH-FLOW COMPRESSOR

机译：高压风力涡轮增压器的高度 - 风 - 隧道 - 高速流动压缩机的性能特征研究 - 高流量压缩机的性能特征

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摘要

A wind tunnel investigation was conducted to determine the performance of a 4000-pound-thrust axial-flow turbojet engine with a high flow compressor. Pressure altitudes included 5000 to 40000 feet with ram pressure ratios from 1.00 to 1.82. Altitudes included 20000 to 40000 feet and ram pressure ratios from 1.09 to 1.75. A comparison is made between engine performance with high flow and low flow compressors.

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作者
William A. Fleming; Richard L. Golladay;
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年度 1948
页码 1-71
总页数 71
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Wind tunnel tests; Turbojet engines; Axial flow; Turbocompressors; Air flow; Thrust; Pressure control; Altitude; Compressors; Performance evaluation;

机译：风洞试验;涡轮喷气发动机;轴流;涡轮压缩机;气流;推力;压力控制;高度;压缩机;性能评估;

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2. Modeling of turbine engine axial-flow compressor and turbine characteristics [J] . M.Orkisz, S.Stawarz Engineering transactions . 1997,第3a4期

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ALTITUDE-WIND-TUNNEL INVESTIGATION OF A 4000-POUND-THRUST AXIAL-FLOW TURBOJET ENGINEⅢ- PERFORMANCE CHARACTERISTICS WITH THE HIGH-FLOW COMPRESSOR

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