The Effectiveness of Wing Vortex Generators in Improving the Maneuvering Characteristics of a Swept-wing Airplane at Transonic Speeds
暂无分享，去创建一个
[1] Jim Rogers Thompson,et al. Flight Calibration of Four Airspeed Systems on a Swept-wing Airplane at Mach Numbers up to 1.04 by the NACA Radar-phototheodolite Method , 1955 .
[2] Howard L Ziff,et al. Flight Determined Buffet Boundaries of Ten Airplanes and Comparisons with Five Buffeting Criteria , 1951 .