Preliminary Flight-Determined Pressure Distributions Over the Wing of the Douglas X-3 Research Airplane at Subsonic and Transonic Mach Numbers

Author: Jordan, Gareth H.
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-H55A10
Link: https://digital.library.unt.edu/ark:/67531/metadc61198/

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