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Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds

Maximum-Lift Investigation of a 1/40-Scale X-1 Airplane Wing at Mach Numbers From 0.60 to 1.15

Maximum-Lift Investigation at Mach Numbers From 0.05 to 1.20 of a Wing With Leading Edge Swept Back 42 Degrees

Effects of rate of flap deflection on flap hinge moment and wing lift through the Mach number range from 0.32 to 0.87

Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds

Wind-Tunnel Investigation at Transonic Speeds of a Jet Control on an 80 Degree Delta-Wing Missile

A wind-tunnel investigation of the development of lift on wings in accelerated longitudinal motion


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