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Digital computer program for generating dynamic turbofan engine models (DIGTEM)This report describes DIGTEM, a digital computer program that simulates two spool, two-stream turbofan engines. The turbofan engine model in DIGTEM contains steady-state performance maps for all of the components and has control volumes where continuity and energy balances are maintained. Rotor dynamics and duct momentum dynamics are also included. Altogether there are 16 state variables and state equations. DIGTEM features a backward-differnce integration scheme for integrating stiff systems. It trims the model equations to match a prescribed design point by calculating correction coefficients that balance out the dynamic equations. It uses the same coefficients at off-design points and iterates to a balanced engine condition. Transients can also be run. They are generated by defining controls as a function of time (open-loop control) in a user-written subroutine (TMRSP). DIGTEM has run on the IBM 370/3033 computer using implicit integration with time steps ranging from 1.0 msec to 1.0 sec. DIGTEM is generalized in the aerothermodynamic treatment of components.
Document ID
19840008117
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Daniele, C. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Krosel, S. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Szuch, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Westerkamp, E. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1983
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-83446
NAS 1.15:83446
E-1748
Report Number: NASA-TM-83446
Report Number: NAS 1.15:83446
Report Number: E-1748
Accession Number
84N16185
Funding Number(s)
PROJECT: RTOP 505-40-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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