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Comparisons of in-flight F-111A inlet performance for on and off scheduled inlet geometry at Mach numbers of 0.68 to 2.18

机译：在马赫数为0.68至2.18时，飞行中F-111a入口和离开预定入口几何形状的入口性能的比较

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摘要

In-flight F-111 data on total and static pressure from left inlet during automatically scheduled and manually controlled off-schedule positioning of spike at Mach 0.68 to 2.18

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作者
Hughes, D. L.; Martin, R. A.;
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年度 1971
页码 1-47
总页数 47
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AUTOMATIC CONTROL; F-111 AIRCRAFT; SUPERSONIC INLETS; TRANSONIC FLIGHT; BOUNDARY LAYER SEPARATION; COMPRESSOR EFFICIENCY; INLET FLOW; PRESSURE RECOVERY; SPIKES (AERODYNAMIC CONFIGURATIONS); VARIABLE GEOMETRY STRUCTURES;

机译：自动控制; F-111飞机;超音速入口;跨音速飞行;边界层分离;压缩机效率;进水流量;压力恢复; spIKEs（空气动力学配置）;可变几何结构;

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Comparisons of in-flight F-111A inlet performance for on and off scheduled inlet geometry at Mach numbers of 0.68 to 2.18

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