Comparison of airfoil sections on two triangular-wing-fuselage configurations at transonic speeds from tests by the NACA wing-flow method

Author: Hall, Albert W.
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51F01
Link: https://digital.library.unt.edu/ark:/67531/metadc59009/

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