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Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine. 7 - Pressure and Temperature Distributions

机译：一个3000磅推力轴流式涡喷发动机的海拔高度，风洞研究。 7 - 压力和温度分布

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年度 1948
页码 p.1-58
总页数 58
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Turbojet engines ; Wind tunnel tests ; Pressure distribution ; Axial flow ; Temperature ; Thrust;

机译：涡轮喷气发动机;风洞试验;压力分布;轴流;温度;推力;

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8. Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine. VII. Pressure and Temperature Distributions [R] . Saari, M. J., Prince, W. R. 1948

机译：3000磅 - 推力轴流涡轮喷气发动机的高度 - 风洞研究。七。压力和温度分布

Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine. 7 - Pressure and Temperature Distributions

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