摘要: The statis stability and control characteristics and air loads on the wing and aileron of a 0.09 scale model of an airplane with a 17 percent thick supercritical wing were investigated. The longitudinal aerodynamic characteristics... 展开
作者 | Ferris, J. C. | ||
---|---|---|---|
原报告号 | N83-11074 | 总页数 | 143 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aerodynamic loads Aerodynamic stability Lateral stability Longitudinal stability Static stability Supercritical wings Ailerons Aircraft models Angle of attack Buffeting Lift Mach number Sideslip Thickness Wind tunnel tests Wing profiles |