Miscellaneous directional-stability data for several airplane-like configurations from rocket-model tests at transonic speeds /

Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like configurations flown as rocket models for other purposes, at transonic speeds, have been collected and compared with the available subsonic and supersonic wind-tunnel data for the same configurations.NACA Research Memorandum L52E06B."September 15, 1952."Title from cover.Includes bibliographical references (p. 9-10).Some approximate values of the yawing moment due to sideslip derivative for eight airplane-like configurations flown as rocket models for other purposes, at transonic speeds, have been collected and compared with the available subsonic and supersonic wind-tunnel data for the same configurations.Mode of access: Internet