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


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