Browse TRAIL Inventories

Experimental Determination of the Effects of Directional Stability and Rotary Damping in Yaw on Lateral Stability and Control Characteristics

The Effect of Lateral Area on the Lateral Stability and Control Characteristics of an Airplane as Determined by Tests of a Model in the Langley Free-Flight Tunnel

Results Obtained During Accelerated Transonic Tests of the Bell XS-1 Airplane in Flights to a Mach Number of 0.92

Preliminary Results of NACA Transonic Flights of the XS-1 Airplane With a 10-Percent-Thick Wing and 8-Percent-Thick Horizontal Tail

Stability and Control Data Obtained from First Flight of X-4 Airplane

Preliminary Theoretical and Flight Investigation of the Lateral Oscillation of the X-1 Airplane

Measurements of Aileron Effectiveness of Bell X-1 Airplane Up to a Mach Number of 0.82

Measurements of Aileron Effectiveness of the Bell X-1 Airplane at Mach Numbers Between 0.9 and 1.06

Elevator-stabilizer effectiveness and trim of the X-1 airplane to a Mach number of 1.06

Effects of the Lateral Oscillation of Fixing the Rudder and Reflexing the Flaps on the Bell X-1 Airplane

Analysis of longitudinal stability and trim of the Bell X-1 airplane at a lift coefficient of 0.3 to Mach numbers near 1.05

Effects on the Snaking Oscillation of the Bell X-1 Airplane of a Trailing-Edge Bulb on the Rudder

Loads experienced in flights of two swept-wing research airplanes in the angle-of-attack range of reduced stability

Aileron and Elevator Hinge Moments of the Bell X-1 Airplane Measured in Transonic Flight

Behavior of the Bell X-1A Research Airplane During Exploratory Flights at Mach Numbers Near 2.0 and at Extreme Altitudes

Comparison of flight and wind-tunnel measurements of high-speed-airplane stability and control characteristics

Simulator studies of jet reaction controls for use at high altitude


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