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Assessing Spontaneous Combustion Instability with Nonlinear Time Series AnalysisConsiderable interest lies in the ability to characterize the onset of spontaneous instabilities within liquid propellant rocket engine (LPRE) combustion devices. Linear techniques, such as fast Fourier transforms, various correlation parameters, and critical damping parameters, have been used at great length for over fifty years. Recently, nonlinear time series methods have been applied to deduce information pertaining to instability incipiency hidden in seemingly stochastic combustion noise. A technique commonly used in biological sciences known as the Multifractal Detrended Fluctuation Analysis has been extended to the combustion dynamics field, and is introduced here as a data analysis approach complementary to linear ones. Advancing, a modified technique is leveraged to extract artifacts of impending combustion instability that present themselves a priori growth to limit cycle amplitudes. Analysis is demonstrated on data from J-2X gas generator testing during which a distinct spontaneous instability was observed. Comparisons are made to previous work wherein the data were characterized using linear approaches. Verification of the technique is performed by examining idealized signals and comparing two separate, independently developed tools.
Document ID
20150016318
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Eberhart, C. J.
(Jacobs Engineering Group, Inc. Huntsville, AL, United States)
Casiano, M. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 24, 2015
Publication Date
June 1, 2015
Subject Category
Numerical Analysis
Spacecraft Propulsion And Power
Report/Patent Number
M15-4311
Report Number: M15-4311
Distribution Limits
Public
Copyright
Public Use Permitted.
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