Theoretical Calculation of the Effect of the Fuselage on the Spanwise Lift Distribution on a Wing

Author: Zlotnick, Martin
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51J19
Link: https://digital.library.unt.edu/ark:/67531/metadc58939/

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