Flight Tests to Determine the Effect of a Fixed Auxiliary Airfoil on the Lift and Drag of a Parasol Monoplane (1932)
NASA Technical Reports Server (NTRS) · leaf 14
Angle of offack of thrust line, degrees, o£ Aerodynamic characteristics of the Fairchild F-22 airplane, with N--22 wing section. Data from ghde tests with propeller locked in vertical position. No correction for propeller dr a g . J
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
