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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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