The effects at transonic speeds of thickening the trailing edge of a wing with a 4-percent-thick circular-arc airfoil

Author: Cleary, Joseph W.
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A51J11
Link: https://digital.library.unt.edu/ark:/67531/metadc59200/

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