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Preliminary investigation of effect on performance of dividing conical-spike nose inlets into halves at Mach numbers 1.5 to 2.0
Author:
Allen, John L.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E55I26
Link:
https://digital.library.unt.edu/ark:/67531/metadc61679/
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