A Study on Improvement of Aerodynamic Characteristics of the Next- Generation SST Wing by Lateral Blowing in Subsonic Flow

Makoto Kamishita; Shigeru Aso; Keiichi Karashima

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A Study on Improvement of Aerodynamic Characteristics of the Next- Generation SST Wing by Lateral Blowing in Subsonic Flow

机译：亚音速流侧吹改善下一代SST机翼气动特性的研究

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An experimental study on the improvement of aerodynamic characteristics of a modified arrow wing by applying lateral blowing in subsonic flow has been conducted. The modified arrow wing, which is one of the baseline configurations of the proto-type of next-generation SST, is selected for the experiments. The testing model is the combination of a body of a circular cylinder and give and a modified arrow wing with aspect ratio of 1.91.

机译：进行了通过在亚音速流中施加侧吹来改善改进型箭翼的空气动力学特性的实验研究。实验选择了改良的箭翼，它是下一代SST原型的基线配置之一。该测试模型是圆柱体和圆柱齿轮以及长宽比为1.91的改进型箭形翼的组合。

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来源
《日本航空宇宙学会論文集》 |2001年第569期|p.174-180|共7页
作者
Makoto Kamishita; Shigeru Aso; Keiichi Karashima;
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原文格式 PDF
正文语种 jpn
中图分类航空;
关键词
aerodynamic characteristics; lateral blowing; flow control;

机译：空气动力学特性侧吹流量控制;

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1. A Study on Improvement of Aerodynamic Characteristics of the Next- Generation SST Wing by Lateral Blowing in Subsonic Flow [J] . Makoto Kamishita, Shigeru Aso, Keiichi Karashima 日本航空宇宙学会論文集 . 2001,第569期

机译：亚音速流侧吹改善下一代SST机翼气动特性的研究
2. A study of high angle of attack aerodynamic characteristics of dalta wing at low speed for development of the next-generation SST [J] . Makoto Kamishita, Shigeru Aso, Yuichi Kumamoto 九州大学工学集報 . 1997,第5期

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
3. Aerodynamic characteristics of flapping wings under steady lateral inflow [J] . Han Jong-Seob, Tuan Nguyen Anh, Han Jae-Hung Journal of Fluid Mechanics . 2019,第期

机译：稳定侧向流入下扑翼的空气动力学特征
4. IMPROVEMENT OF AERODYNAMIC CHARACTERISTICS OF NEXT-GENERATION SST WING BY LATERAL BLOWING [C] . M. Kamishita, S. Aso, K. Karashima, 22nd international congress of aeronautical sciences (ICAS 2000) . 2000

机译：侧吹法改善下一代SST机翼的气动特性
5. A theoretical and computational study on the effects of leading edge lateral blowing on delta wing aerodynamics. [D] . Hong, John Suh. 1994

机译：对前缘横向吹气对三角翼空气动力学影响的理论和计算研究。
6. Improvement of the aerodynamic performance by wing flexibility and elytra–hind wing interaction of a beetle during forward flight [O] . Tuyen Quang Le, Tien Van Truong, Soo Hyung Park, 2013

机译：甲虫在前飞过程中的机翼灵活性和鞘翅与后翅的相互作用改善了空气动力学性能
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

机译：亚源流动横向吹塑改善下一代SST翼的空气动力学特性的研究。
8. The subsonic static aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3. II : lateral and directional characteristics [R] . Savage, Howard F, Tinling, Bruce E 1957

机译：具有纵横比为3的三角翼的飞机模型的亚音速静态空气动力学特性.II：横向和方向特性

A Study on Improvement of Aerodynamic Characteristics of the Next- Generation SST Wing by Lateral Blowing in Subsonic Flow

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