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Wind-Tunnel Tests of a 1/6-Scale Model of Republic XF-12 Vertical Tail with Stub Fuselage and Stub Horizontal Tail.

机译：共和国XF-12垂直尾翼1/6比例模型的风洞试验，带有短柱机身和短柱水平尾翼。

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摘要

A 1/6-scale model of the Republic XF-12 vertical tail with stub fuselage and stub horizontal tail was tested in the Langley stability tunnel to determine the aerodynamic characteristics of the model, The investigation included a study of the effects of bo ...

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作者
R. MacLachlan;
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年度 1945
页码 1-55
总页数 55
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Angle of attack; Asymmetry; Boundary layer thickness; Engine failure; Fillets; Fuselages; Horizontal tail surfaces; Lift; Multiengine vehicles; Republic aircraft; Rudders; Scale models; Wind tunnel tests;

机译：攻角;不对称;边界层厚度;发动机故障;圆角;保险丝;水平尾翼;升力;多发车辆;共和国飞机;舵;比例模型;风洞试验;

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3. Experimental and Computational Analysis of Model–Support Interference in Low-Speed Wind-Tunnel Testing of Fuselage-Boundary-Layer Ingestion [J] . Biagio Della Corte, André A.V. Perpignan, Martijn van Sluis, MATEC Web of Conferences . 2019,第3期

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Wind-Tunnel Tests of a 1/6-Scale Model of Republic XF-12 Vertical Tail with Stub Fuselage and Stub Horizontal Tail.

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