Formulas for the Supersonic Loading, Lift, and Drag of Flat Swept-Back Wings With Leading Edges Behind the Mach Line

Author: Cohen, Doris
Year: 1950
Document Type: N/A
Series: NACA Technical Reports
Report Number: NACA-TR-1050
Link: https://digital.library.unt.edu/ark:/67531/metadc60392/

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