Natural-laminar-flow airfoil development for a lightweight business jet

被引：71

作者：

Fujino, M ^{[1
]}

Yoshizaki, Y ^{[1
]}

Kawamura, Y ^{[1
]}

机构：

[1] Honda R&D Amer Inc, Greensboro, NC 27409 USA

来源：

JOURNAL OF AIRCRAFT | 2003年 / 40卷 / 04期

关键词：

D O I：

10.2514/2.3145

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A 15% thick, natural-laminar-flow airfoil, the SHM-1, has been designed to satisfy requirements derived from the performance specifications for a lightweight business jet. The airfoil was tested in a low-speed wind tunnel to evaluate its low-speed performance. A flight test was also conducted to evaluate the performance of the airfoil at high Reynolds numbers and high Mach numbers. In addition, a transonic wind-tunnel test was conducted to determine the drag-divergence characteristics. The design requirements, methodology, and experimental verification are described.

引用

页码：609 / 615

页数：7

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