Browse TRAIL Inventories

Wind-tunnel investigation of perforated split flaps for use as dive brakes on a rectangular NACA 23012 airfoil

Aerodynamic characteristics and flap loads of perforated double split flaps on a rectangular NACA 23012 airfoil

Aerodynamic Characteristics of Several Modifications of a 0.45-Scale Model of the Vertical Tail of the Curtiss XP-62 Airplane

Preliminary Investigation of Various Ailerons on a 42 Degree Sweptback Wing for Lateral Control at Transonic Speeds

Aerodynamic characteristics at subsonic and transonic speeds of a 42.7 degree sweptback wing model having an aileron with finite trailing-edge thickness

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


Published Year

Subject

Author