Development of dynamic simulation of TF34-GE-100 turbofan engine with post-stall capabilityThis paper describes the development of a hybrid computer simulation of a TF34-GE-100 turbofan engine with post-stall capability. The simulation operates in real-time and will be used to test and evaluate stall recovery control modes for this engine. The simulation calculations are performed by an analog computer with a peripheral multivariable function generation unit used for computing bivariate functions. Tabular listings of simulation variables are obtained by interfacing to a digital computer and using a custom software package for data collection and display.
Document ID
19840061391
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Krosel, S. M. (NASA Lewis Research Center Cleveland, OH, United States)