ROLLING PULLOUT STUDY. PARTⅡ:FLIGHT MEASUREMENT OF VERTICAL AND HORIZONTAL TAIL LOADS DURING A RUDDER LOCKED ROLLING PULLOUT MANEUVER

摘要

In addition to these basic quantities, recorded time histories of the control inputs, rolling and yawing velocities, sideslip angle, normal acceleration, and forward speed change are presented.nThe tests were made under a variety of geometric and aerodynamic configurations. Such quantities as load factor, Mach number, o.g. position, altitude and lateral moments of inertia were varied in order to present as complete a picture as possible of the responses to be expected under various plausible conditions.