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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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