Investigation of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel V : static longitudinal stability and control throughout the subsonic speed range of a semispan model of a supersonic airplane
Description: No Description Available.
Date: December 8, 1949
Creator: Johnson, Ben H , Jr & Rollins, Francis W
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department