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 Technical Notes
Report Number: NACA-TN-1319
Link: https://digital.library.unt.edu/ark:/67531/metadc55502/

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