An experimental investigation of reduction in transonic drag rise at zero lift by the addition of volume to the fuselage of a wing-body-tail configuration and a comparison with theory

Author: Holdaway, George H.
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A54F22
Link: https://digital.library.unt.edu/ark:/67531/metadc62752/

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