Validity Check of the Assessment of a Jet Turbine Engine Regulation in Flight Using a Computer Simulation

Karol Golak

doi:10.4028/www.scientific.net/SSP.199.123

Paper Titles

Harmonic Balance Analysis for the Rigid Finite Element Model of the Rotating Cracked Shaft
p.99

Simulation-Based Study on the Dynamics of Wing-Flap Actuating Hydraulic Circuit
p.105

Statistical Diagnostic Thresholds of Rolling Bearings with Correlation of the Bearings Signal and its Environment Based on Cauchy Product
p.111

The Analysis of Finishing Tooling Influence on Contact Fatigue Researched by Profilometer
p.117

Validity Check of the Assessment of a Jet Turbine Engine Regulation in Flight Using a Computer Simulation
p.123

An Application for Analysis of Temperature during Cold Rolling
p.131

Effect of Temperature and Deformation Rate on the Dynamic Viscosity of Ferrofluid
p.137

Graph-Based Models of Compound Planetary Gear Boxes
p.143

Measuring and Analyzing the Moment of Friction in Double-Row Ball Bearings
p.149

HomeSolid State PhenomenaSolid State Phenomena Vol. 199Validity Check of the Assessment of a Jet Turbine...

Validity Check of the Assessment of a Jet Turbine Engine Regulation in Flight Using a Computer Simulation

Abstract:

In this paper, a method of evaluation of the turbojet engine regulation condition in flight, based on information from its ground tests was presented. The tested engine was presented by the single comprehensive model which links input (in form of the modified signal mp4) and engine output (in form of the modified signal np2). Changes of the model parameters following during its operation can be defined using changes of the proposed simulation model parameters describing the engine operation both in flight and during ground tests.

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Periodical:

Solid State Phenomena (Volume 199)

Pages:

123-128

DOI:

https://doi.org/10.4028/www.scientific.net/SSP.199.123

Citation:

Cite this paper

Online since:

March 2013

Authors:

Karol Golak

Keywords:

Computer Simulation, Ground Tests, Parametrical Diagnostic, Regulation, Turbine Jet Engine

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