“…According to Woan et al 1991, Anderson & Bohn-Meyer 1992, and Norris 1994, the suction glove on the F-16XL Ship 1 was designed for a Mach n umber of 1.6, altitude of 44000 ft, angle of attack o f 2 o , momentum thickness Reynolds number on the attachment line of less than 114, and a unit Reynolds numb e r o f 2 : 53 10 6 ft. Suction was limited to the rst 25 chord and attachment-line CF disturbances were the primary focus of the LFC experiment Figure 5.…”