Investigation of symmetric body indentations designed to reduce the transonic zero-lift wave drag of a 45 degree swept wing with an NACA 64A006 section and with a thickened leading-edge section

Author: Holdaway, George H
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A56K26
Link: https://digital.library.unt.edu/ark:/67531/metadc63309/

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