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Interference effects at Mach 1.9 on a horizontal tail due to trailing shock waves from an axisymmetric body with an exiting jet
Author:
Salmi, Reino J.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E55J13a
Link:
https://digital.library.unt.edu/ark:/67531/metadc61747/
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