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Drag Measurements of Symmetrical Circular-Arc and NACA 65-009 Rectangular Airfoils Having an Aspect Ratio of 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-L6J14
Link:
https://digital.library.unt.edu/ark:/67531/metadc58087/
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