Drag Measurements of a 34 Degree Swept-Forward and Swept-Back NACA 65-009 Airfoil of Aspect Ratio 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-L6I11
Link: https://digital.library.unt.edu/ark:/67531/metadc58039/

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