Lift and drag characteristics of the Douglas D-558-II research airplane obtained in exploratory flights to a Mach number of 2.0

Author: Nugent, Jack
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L54F03
Link: https://digital.library.unt.edu/ark:/67531/metadc60393/

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