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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