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Measurements of the Pressure Distribution on the Horizontal Tail Surface of a Typical Propeller-Driven Pursuit Airplane in Flight 2: The Effect of Angle of Sideslip and Propeller Operation

Measurements of the Pressure Distribution on the Horizontal-Tail Surface of a Typical Propeller-Driven Pursuit Airplane in Flight 1: Effects of Compressibility in Steady Straight and Accelerated Flight

Preliminary Results of a Flight Investigation to Determine the Effect of Negative Flap Deflection on High-Speed Longitudinal-Control Characteristics

Measurements of the Pressure Distribution on the Horizontal-Tail Surface of a Typical Propeller-Driven Pursuit Airplane in Flight 3: Tail Loads in Abrupt Pull-Up Push-Down Maneuvers

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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