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Exploratory investigation of the effect of wing slots and leading-edge slats on the longitudinal stability characteristics of a 45 degree sweptback wing-fuselage configuration

机译：翼槽和前缘缝翼对45度后掠翼 - 机身构型纵向稳定特性影响的探索性研究

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作者
Critzos, Chris C;
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年度 1957
页码 1-35
总页数 35
原文格式 PDF
正文语种 eng
中图分类工业技术;
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专利

1. Leading-Edge Radius Effects on Aerodynamic Characteristics of 50-Degree Delta Wings [J] . N. G. Verhaagen Journal of Aircraft . 2012,第2期

机译：前沿半径对50度三角翼气动特性的影响
2. Investigation and Improvement of Stall Characteristic of High-Lift Configuration without Slats [J] . Yang Zhao, Li Jie, Jin Jing, International journal of aerospace engineering . 2019,第PTa4期

机译：没有板条的高升力配置的调查和改进
3. Investigation and Improvement of Stall Characteristic of High-Lift Configuration without Slats [J] . Zhao Yang, Jie Li, Jing Jin, International journal of aerospace engineering . 2019,第4期

机译：没有板条的高升力配置的调查和改进
4. Numerical and Experimental Investigation of the Sound Generation in a Slat Cove of a High- Lift Wing Configuration [C] . S. Becker, F. Schaefer, C. Scheit, AIAA/CEAS Aeroacoustics Conference;AIAA Aeroacoustics Conference . 2008

机译：高升力机翼板条槽内发声的数值和实验研究
5. Some experiments on the flow in the boundary layer of a 45 degrees sweptback untapered wing of aspect ratio 4 [O] . Emslie K., Hosking L., Marshall W. S. D. 1953

机译：纵横比为4的45度后掠无锥翼边界层流动的一些实验

Exploratory investigation of the effect of wing slots and leading-edge slats on the longitudinal stability characteristics of a 45 degree sweptback wing-fuselage configuration

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