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Large-scale wind tunnel tests of a subsonic transport with AFT engine nacelles and high tail

机译：aFT发动机短舱和高尾部亚音速运输的大型风洞试验

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摘要

Static longitudinal stability and control at angles of attack above those for wing stall in large-scale subsonic transport model

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作者
Aoyagi, K.; Tolhurst, W. H., Jr.;
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年度 1967
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
AERODYNAMIC STALLING; AIRCRAFT MODELS; ANGLE OF ATTACK; FUSELAGES; LONGITUDINAL CONTROL; LONGITUDINAL STABILITY; NACELLES; STATIC AERODYNAMIC CHARACTERISTICS; STATIC STABILITY; SUBSONIC AIRCRAFT; SUBSONIC SPEED; WIND TUNNEL TESTS; AIRCRAFT MODEL; LONGITUDINAL STABILITY AND CONTROL; STATIC AERODYNAMIC CHARACTERISTICS; SUBSONIC AIRCRAFT;

机译：空气动力学失败;飞机模型;攻击角度;机身;纵向控制;纵向稳定性;发动机舱;静态空气动力学特性;静态稳定性; sUBsONIC aIRCRaFT; sUBsONIC spEED;风洞隧道测试;飞机模型;纵向稳定性和控制;静态空气动力学特性; sUBsONIC aIRCRaFT;

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8. Large-Scale Wind Tunnel Tests of a Subsonic Transport with Aft Engine Nacelles and High Tail [R] . Aoyagi, K., Tolhurst, W. H. 1967

机译：具有尾部发动机短舱和高尾部的亚音速运输的大型风洞试验

Large-scale wind tunnel tests of a subsonic transport with AFT engine nacelles and high tail

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