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Drag characteristics of rectangular and swept-back NACA 65-009 airfoils having aspect ratios of 1.5 and 2.7 as determined by flight tests at supersonic speeds
Author:
Alexander, Sidney R.
Year:
1947
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L6J16
Link:
https://digital.library.unt.edu/ark:/67531/metadc58091/
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