Investigation of Minimum Drag and Maximum Lift-Drag Ratios of Several Wing-Body Combinations Including a Cambered Triangular Wing at Low Reynolds Numbers and at Supersonic Speeds

Author: Brown, Clinton E.
Year: 1958
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-4020
Link: https://digital.library.unt.edu/ark:/67531/metadc57343/

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