Some Effects of Frequency on the Contribution of a Vertical Tail to the Free Aerodynamic Damping of a Model Oscillating in Yaw
Statistical Analysis of Spherical Data
Memorial and biographical history of Ellis county, Texas
Some Effects of Frequency on the Contribution of a Vertical Tail to the Free Aerodynamic Damping of a Model Oscillating in Yaw
Approximate Corrections for the Effects of Compressibility on the Subsonic Stability Derivatives of Swept Wings
Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60° Delta-wing Airplane Model
Equations and Charts for Determining the Hypersonic Stability Derivatives of Combinations of Cone Frustums Computed by Newtonian Impact Theory
Experimental Determination of Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Unswept Wing Oscillating in Yaw
An Investigation of the Effect of Vertical-fin Location and Area on Low-speed Lateral Stability Derivatives of a Semitailless Airplane Model
Experimental Determination of the Aerodynamic Derivatives Arising from Acceleration in Sideslip for a Triangular, a Swept, and an Unswept Wing
Low-speed Static Longitudinal and Lateral Stability Characteristics of Two Low-aspect-ratio Wings Cambered and Twisted to Provide a Uniform Load at a Supersonic Flight Condition
Investigation of Several Blunt Bodies to Determine Transonic Aerodynamic Characteristics Including Effects of Spinning and of Extendible Afterbody Flaps and Some Measurements of Unsteady Base Pressures
Experimental Determination of the Effects of Frequency and Amplitude on the Lateral Stability Derivatives for a Delta, a Swept, and an Unswept Wing Oscillating in Yaw
An Investigation of the Contribution of the Vertical Tail to the Lateral Damping of an Airplane Oscillating in Yaw
Aerodynamic Characteristics of Some Families of Blunt Bodies at Transonic Speeds [with List of References]
Thirty-ninth Annual Report of the National Advisory Committee for Aeronautics, 1953. Including Technical Reports Nos. 1111 to 1157
Some Effects of Aspect Ratio and Tail Legth on the Contribution of a Vertical Tail to Unsteady Lateral Damping and Directional Stability of a Model Oscillating Continuously in Yaw
Effect of Taper Ratio on the Low-speed Rolling Stability Derivatives of Swept and Unswept Wings of Aspect Ratio 2.61
Thirty-sixth Annual Report of the National Advisory Committee for Aeronautics, 1950. Including Technical Reports Nos. 951 to 1002