Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 2.46 and 3.36

Author: Kaattari, George E.
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A54J12
Link: https://digital.library.unt.edu/ark:/67531/metadc60859/

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