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Investigation at Supersonic Speeds of the Effect of Jet Mach Number and Divergence Angle of the Nozzle Upon the Pressure of the Base Annulus of a Body of Revolution
Author:
Bromm, August F., Jr.
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L54I16
Link:
https://digital.library.unt.edu/ark:/67531/metadc60964/
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