Flight-determined pressure distributions over a section of the 35 degree swept wing of the Douglas D-558-II research airplane at Mach numbers up to 2.0

Author: Jordan, Gareth H.
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-H55A03
Link: https://digital.library.unt.edu/ark:/67531/metadc61081/

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