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 15
\ Fig. 5 N.A.C.A. Technical Note No.440 2.2 LI 22 … Angle of attack of thrust line, degrees, oS Fig. 5 Aerodynamic characteristics of the Fairchild F-22 airplane fitted with aii auxiliary airfoil on an N-22 wing, based on mam wing area only. Data from glide tests with propeller locked in vertical position. liO correction for drag of propeller.
NASA Technical Reports Server (NTRS)
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