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High frequency dynamic engine simulationA digital computer simulation of a mixed flow, twin spool turbofan engine was assembled to evaluate and improve the dynamic characteristics of the engine simulation to disturbance frequencies of at least 100 Hz. One dimensional forms of the dynamic mass, momentum and energy equations were used to model the engine. A TF30 engine was simulated so that dynamic characteristics could be evaluated against results obtained from testing of the TF30 engine at the NASA Lewis Research Center. Dynamic characteristics of the engine simulation were improved by modifying the compression system model. Modifications to the compression system model were established by investigating the influence of size and number of finite dynamic elements. Based on the results of this program, high frequency engine simulations using finite dynamic elements can be assembled so that the engine dynamic configuration is optimum with respect to dynamic characteristics and computer execution time. Resizing of the compression systems finite elements improved the dynamic characteristics of the engine simulation but showed that additional refinements are required to obtain close agreement simulation and actual engine dynamic characteristics.
Document ID
19780005116
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Schuerman, J. A.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Fischer, K. E.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Mclaughlin, P. W.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
PWA-5543
NASA-CR-135313
Report Number: PWA-5543
Report Number: NASA-CR-135313
Accession Number
78N13059
Funding Number(s)
CONTRACT_GRANT: NAS3-20292
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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