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- 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