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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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