Free-flight investigation at transonic speeds of drag coefficients of a boattail body of revolution with a simulated turbojet exhaust issuing at the base from conical short-length ejectors

Author: Falanga, Ralph A.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L56H23
Link: https://digital.library.unt.edu/ark:/67531/metadc63107/

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