Experimental Effects of Propulsive Jets and Afterbody Configurations on the Zero-Lift Drag of Bodies of Revolution at a Mach Number of 1.59

Author: de Moraes, Carlos A.
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L54C16
Link: https://digital.library.unt.edu/ark:/67531/metadc60364/

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