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Calculations of the Supersonic Wave Drag of Nonlifting Wings with Arbitrary Sweepback and Aspect Ratio: Wings Swept Behind the Mach Lines
Author:
Harmon, Sidney M.
Year:
1947
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L6K29
Link:
https://digital.library.unt.edu/ark:/67531/metadc58100/
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