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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