首页> 美国政府科技报告 >PRELIMINARY RESULTS OF AN ALTITUDE-WIND-TUNNEL INVESTIGATION OF AN AXIAL-FLOW GAS TURBINE-PROPELLER ENGINEⅡ- WINDMILLING CHARACTERISTICS

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PRELIMINARY RESULTS OF AN ALTITUDE-WIND-TUNNEL INVESTIGATION OF AN AXIAL-FLOW GAS TURBINE-PROPELLER ENGINEⅡ- WINDMILLING CHARACTERISTICS

机译：轴流式燃气轮机 - 螺旋桨发动机Ⅱ-风力发电特性的高海拔隧道研究初步结果

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Wind tunnel investigations were performed to determine the performance properties of an axial-flow gas turbine-propeller engine II. Windmilling characteristics were determined for a range of altitudes from 5000 to 35,000 feet, true airspeeds from 100 to 273 miles per hour, and propeller blade angles from 4 degrees to 46 degrees.

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作者
E. W. Conrad; J. D. Durham;
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年度 1948
页码 1-53
总页数 53
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Wind tunnel tests; Axial flow; Gas turbines; Propellers; Altitude; Turbine engines; Propeller blades; Airspeed; Windmilling;

机译：风洞试验;轴向流动;燃气轮机;螺旋桨;高度;涡轮发动机;螺旋桨叶片;空速;风车;
入库时间 2022-08-29 11:20:18

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PRELIMINARY RESULTS OF AN ALTITUDE-WIND-TUNNEL INVESTIGATION OF AN AXIAL-FLOW GAS TURBINE-PROPELLER ENGINEⅡ- WINDMILLING CHARACTERISTICS

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