Lifting-Surface-Theory Results for Thin Elliptic Wings of Aspect Ratio 3 with Chordwise Loadings Corresponding to 0.5-Chord Plain Flap and to Parabolic-Arc Camber

Author: Crandall, Stewart M.
Year: 1946
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-1064
Link: https://digital.library.unt.edu/ark:/67531/metadc54789/

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