NASA NACA-RM-L52L05-1952 当雷诺数为2.50x10(指数6)至8.10x10(指数6)时,通过在展弦比为6的37°后掠翼上可渗透前沿上的抽吸风洞研究
Wind-tunnel investigation of stall control by suction through a porous leading edge on a 37 degrees sweptback wing of aspect ratio 6 at Reynolds numbers from 2.50 x 10(exp 6) to 8.10 x 10(exp 6)