Force and pressure-recovery characteristics of a conical-type nose inlet operating at Mach numbers of 1.6 to 2.0 and at angles of attack to 9 degrees

Author: Beke, Andrew
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E52I30
Link: https://digital.library.unt.edu/ark:/67531/metadc59415/

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