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Flight Tests to Determine the Effect of Airfoil Section Profile and Thickness Ratio on the Zero-Lift Drag of Low-Aspect-Ratio Wings at Supersonic Speeds
Author:
Katz, Ellis
Year:
1948
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L7K14
Link:
https://digital.library.unt.edu/ark:/67531/metadc58150/
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