NASA NTRS · 19860000242
HYTESS-Hypothetical Turbofan-Engine Simplified Simulation
Abstract
Simulated characteristics mimic those of advanced turbofan engines. Computer program developed to offer those interested in engine dynamics and controls research efficient, realistic, and easily-used engine simulation. Simulation developed from linearized operating-point models but still retains essential nonlinear engine effects. Representative of hypothetical, low-bypass-ratio, twin-spool, axialflow turbofan engine. Program written in FORTRAN IV.
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Merrill, W., Beattie, C., Laprad, R., Rock, S., Akhter, M.. 1986-05-01. HYTESS-Hypothetical Turbofan-Engine Simplified Simulation. https://ntrs.nasa.gov/citations/19860000242
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