NASA Rotor 37 zCFD Code Validation - Flow Field in a Transonic Axial Compressor
Authors: A. Cimpoeru (CFMS), J. Appa (Zenotech) and D. Standingford (Zenotech)
Geometry and Mesh Generation (NASA ROTOR37)
Initial Conditions (Steady-State RANS)
Inflow Total Conditions.
Note that the map has been initially generated by varying the static pressure ratio on the outflow from 0.7 to 1.8 in order to determine the chocked and stalled conditions.
More results will be publised in the following weeks.