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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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