Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
7 results returnedSearch results
- 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