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Experimental investigation of effects of primary jet flow and secondary flow through a zero-length ejector on base and boattail pressures of a body of revolution at free-stream Mach numbers of 1.62, 1.93, and 2.41
Author:
O'Donnell, Robert M.
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L54I22
Link:
https://digital.library.unt.edu/ark:/67531/metadc62710/
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