Pressure Distributions at Mach Numbers From 0.6 to 1.9 Measured in Free Flight on a Parabolic Body of Revolution With Sharply Convergent Afterbody

Author: Stoney, William E., Jr.
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51L03
Link: https://digital.library.unt.edu/ark:/67531/metadc59901/

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