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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