NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
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)
Date Acquired
August 12, 2013
Publication Date
June 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 84-1184
Accession Number
84A44178
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available