A Turbojet Simulator for Mach Numbers up to 2.0
Author(s) -
Fred W Steffen,
E. A. Satmary,
M. R. Vanco,
S. M. Nosek
Publication year - 1972
Publication title -
nasa sti repository (national aeronautics and space administration)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.1115/72-gt-89
Subject(s) - transonic , nozzle , aerodynamics , mach number , turbine , gas compressor , turbojet , simulation , aerospace engineering , wind tunnel , engineering , flow (mathematics) , automotive engineering , mechanical engineering , marine engineering , mechanics , physics
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