NASA NACA-RM-L9E24-1949 当雷诺数为6,800,000时,带有前缘42°后掠角带有或不带高升力装置的低速副翼控制特性的研究
Investigation of low-speed aileron control characteristics at a Reynolds number of 6,800,000 of a wing with leading edge swept back 42 degrees with and without high-lift devices