原文传递
Rotary balance data for a single engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 deg to 90 deg
| 题名： | Rotary balance data for a single engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 deg to 90 deg |
| 作者： | Mulcay, W. J.; Rose, R. |
| 关键词： | balance；aspect；attac；design；single；range；engine；characteristics；gener；data |
| 摘要： | Aerodynamic characteristics obtained in a helical flow environment utilizing a rotary balance located in the Langley spin tunnel are presented in plotted form. The configurations tested included the basic airplane, various control deflections, two canard locations, and wing leading edge modifications, as well as airplane components. |
| 报告类型： | 科技报告 |
相关文献
- Crash tests of three identical low-wing single-engine airplane
- Crash tests of four low-wing twin-engine airplanes with truss-reinforced fuselage structure
- Light airplane crash tests at three pitch angles
- Light airplane crash tests at three roll angles
- Experimental and Numerical Analysis of Triaxially Braided Composites Utilizing a Modified Subcell Modeling Approach.
- Experimental and Numerical Analysis of Triaxially Braided Composites Utilizing a Modified Subcell Modeling Approach.
检索历史
应用推荐
