Full-Scale Wind-Tunnel Investigation of Wing-Cooling Ducts Effects of Propeller Slipstream, Special Report
Description:
Report presenting an investigation of finite span wing-cooling ducts that has been extended to include a study of the effects of slipstream on the duct characteristics. The results indicated that the propeller slipstream is effective in generating a flow of air through the ducts of the ground condition.
Date:
March 1939
Creator:
Nickle, F. R. & Freeman, Arthur B.
Partner:
UNT Libraries Government Documents Department