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Stall Characteristics Obtained from Flight 10 of Northrop X-4 No. 2 Airplane (USAF No. 46-677)

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

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

Flight measurements of the horizontal-tail loads on a swept-wing fighter airplane at transonic speeds

On the use of a damped sine-wave elevator motion for computing the design maneuvering horizontal-tail load

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

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

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


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