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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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