Aerodynamic Characteristics of Four Bodies of Revolution Showing Some Effects of Afterbody Shape and Fineness Ratio at Free-Stream Mach Numbers From 1.50 to 1.99

Author: Cohen, Robert J.
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E51C06
Link: https://digital.library.unt.edu/ark:/67531/metadc58810/

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