Large-Scale Boundary-Layer Control Tests on Two Wings in the NACA 20-Foot Wind Tunnel, Special Report
Description:
Report discussing tests performed on two different wings to determine the increase in lift obtainable by removing the boundary layer and power required for the blower. The results for the stub wing were more favorable than the large-span wing.
Date:
April 1935
Creator:
Freeman, Hugh B.
Partner:
UNT Libraries Government Documents Department