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A simple propulsion system model for the simulation of nonlinear dynamic thrust response

Author
Krauspe, P.
Published
Mar 1, 1983.
Physical Description
1 electronic document
Additional Creators
Schaenzer, G.
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
A simple mathematical jet engine description is presented where the measured transition functions of the engine thrust can be simulated in a quasi-stationary operation as well as in acceleration or deceleration schedules. Because of its simplicity and high fidelity, it is especially suited for representing jet engines in digital simulation programs.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19830015039.
Accession ID: 83N23310.
NASA-TM-77053.
NAS 1.15:77053.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15712801