Theory and Preliminary Flight Tests of an All-Movable Vertical Tail Surface
Theoretical study of air forces on an oscillating or steady thin wing in a supersonic main stream
Some considerations on an airfoil in an oscillating stream
Sideslip angles and vertical-tail loads developed by periodic control deflections
Response of a helicopter rotor to oscillatory pitch and throttle movements
On the stability of oscillations of an airplane wing
Flight Tests of an Airplane Model with a 62 Degree Swept-back Wing in the Langley Free-flight Tunnel
First-order theory for unsteady motion of thin wings at supersonic speeds
Effect of steady rolling on longitudinal and directional stability