A study of high angle of attack aerodynamic characteristics of dalta wing at low speed for development of the next-generation SST

Makoto Kamishita; Shigeru Aso; Yuichi Kumamoto

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A study of high angle of attack aerodynamic characteristics of dalta wing at low speed for development of the next-generation SST

机译：低速达达机翼大迎角空气动力学特性研究以开发下一代SST

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Recently, the configuration of main wing of the next-generation SST(Super-Sonic Trans- port), which is the improvement of Arrow Wing Configuration, has been decided. However, the performance in low speed is not understood sufficiently. In this paper the experiment using several configuration-models, SST Arrow Model, Double Delta Model and Delta Model, has been conducted in the low speed wind tunnel at Reynolds numbers of 6.2 x 10~5. The difference of high-angle of attack aerodynamic characteristics in those configurations has been revealed.

机译：最近，已经确定了下一代SST（超音速运输）的主翼配置，这是Arrow Wing配置的改进。但是，对低速性能的理解不够。本文在雷诺数为6.2 x 10〜5的低速风洞中使用几种配置模型（SST箭头模型，双三角模型和三角模型）进行了实验。揭示了在那些配置中高攻角空气动力学特性的差异。

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来源
《九州大学工学集報》 |1997年第5期|p.527-532|共6页
作者
Makoto Kamishita; Shigeru Aso; Yuichi Kumamoto;
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原文格式 PDF
正文语种 jpn
中图分类工业技术;
关键词
SST; arrow wing; delta wing;

机译：SST;箭翼三角翼;

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5. Aerodynamic control of a wing at low angles of attack using synthetic jets and Gurney flaps. [D] . Shea, Patrick R. 2008

机译：使用合成射流和格尼襟翼以低攻角对机翼进行空气动力学控制。
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7. A Study on Improvement of Aerodynamic Characteristics of the Next-Generation SST Wing by Lateral Blowing in Subsonic Flow. [O] . Makoto KAMISHITA, Shigeru ASO, Keiichi KARASHIMA, 2001

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8. An experimental investigation of the effect of Reynolds number on the low speed aerodynamic characteristics of a delta wing space shuttle orbiter concept at angles of attack to 45 degrees [R] . Parrell, H. 1971

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A study of high angle of attack aerodynamic characteristics of dalta wing at low speed for development of the next-generation SST

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