Zobrazeno 1 - 1
of 1
pro vyhledávání: '"Serhad Aytac"'
Publikováno v:
Volume 10: Fluids Engineering.
In this study, jet temperature effects on afterbody drag in subsonic, transonic and supersonic flow conditions have been investigated for a wide range of nozzle throat total pressure to free-stream static pressure ratio (NPR) at Mach numbers 0.6, 0.9