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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