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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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