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- Longitudinal-stability characteristics of the Northrop X-4 airplane (USAF No. 46-677)
- Summary report of results obtained during demonstration tests of the Northrop X-4 airplanes
- Stall Characteristics Obtained from Flight 10 of Northrop X-4 No. 2 Airplane (USAF No. 46-677)
- Stability and Control Measurements Obtained during USAF-NACA Cooperative Flight-Test Program on the X-4 Airplane (USAF No. 46-677)
- Flight Investigation of the Longitudinal Stability and Control Characteristics of the Douglas D-558-I Airplane (BuAero No. 37972) at Mach Numbers Up to 0.89
- On the use of a damped sine-wave elevator motion for computing the design maneuvering horizontal-tail load
- Flight measurements of the horizontal-tail loads on a swept-wing fighter airplane at transonic speeds
- The Effect of Blunt-Trailing-Edge Modifications on the High-Speed Stability and Control Characteristics of a Swept-Wing Fighter Airplane
- A flight evaluation of the stability and control of the X-4 swept-wing semitailless airplane
- Summary of the flight conditions and maneuvers in which maximum wing and tail loads were experienced on a swept-wing fighter airplane
- A method for evaluating the loads and controllability aspects of the pitch-up problem
- Summary of the Flight Conditions and Maneuvers in Which Maximum Wing and Tail Loads Were Experienced on a Swept-Wing Fighter Airplane
- Analytical study of the comparative pitch-up behavior of several airplanes and correlation with pilot opinion
- An analytical evaluation of the effects of an aerodynamic modification and of stability augmenters on the pitch behavior and probable pilot opinion of two current fighter airplanes