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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