Show/Hide Menu
Hide/Show Apps
Logout
Türkçe
Türkçe
Search
Search
Login
Login
OpenMETU
OpenMETU
About
About
Open Science Policy
Open Science Policy
Open Access Guideline
Open Access Guideline
Postgraduate Thesis Guideline
Postgraduate Thesis Guideline
Communities & Collections
Communities & Collections
Help
Help
Frequently Asked Questions
Frequently Asked Questions
Guides
Guides
Thesis submission
Thesis submission
MS without thesis term project submission
MS without thesis term project submission
Publication submission with DOI
Publication submission with DOI
Publication submission
Publication submission
Supporting Information
Supporting Information
General Information
General Information
Copyright, Embargo and License
Copyright, Embargo and License
Contact us
Contact us
Investigation of a Solution Approach to Quadratic Eigenvalue Problem for Thermoacoustic Instabilities
Date
2022-01-01
Author
Öztürkmen, Musa Onur
Özyörük, Yusuf
Metadata
Show full item record
This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
.
Item Usage Stats
211
views
0
downloads
Cite This
© 2022, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.The interactions between the unsteady heat release and pressure fluctuations in a combustion chamber may lead to thermoacoustic instabilities. Linear stability characteristics of the chamber may be determined by solving the nonhomogeneous wave equation in frequency domain that takes these interactions into account. The discretization of the wave equation with frequency-dependent source terms due to heat release and impedance boundary conditions results in a nonlinear quadratic eigenvalue problem. While the solution of the standard linear quadratic eigenvalue problem can be obtained directly, the nonlinear one requires some linearization procedures to reduce it to the standard general eigenvalue problem. In this paper, three different linearization procedures are investigated. For validation of the considered approaches a canonical problem that contains impedance walls and uniformly distributed heat source is set up and solved analytically. An experimental experimental test case from literature is also considered to assess the utilized linearization methods in terms of convergence and CPU times. It is shown that among the employed linearization approaches, the Taylor series based one yields faster convergence.
URI
https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85123608792&origin=inward
https://hdl.handle.net/11511/97559
DOI
https://doi.org/10.2514/6.2022-1855
Conference Name
AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Collections
Department of Aerospace Engineering, Conference / Seminar
Suggestions
OpenMETU
Core
Analysis of effects of different diffusion models in hypersonic flow regimes
Gur, H. Berk; Eyi, Sinan (2017-01-01)
© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.Hypersonic flows become popular due to its use in space explorations and military applications. It occurs normally, when a space craft re-enter to the atmosphere. Space crafts are exposed to high temperatures and high pressures because of Earth’s atmosphere and gravity. In addition in high temperatures, gases tend to react with each other. These reactions also have effects on space craft’s surface. In order to calculat...
Analysis of hypersonic flow using three dimensional Navier-Stokes equations
Özgün, Muharrem; Eyi, Sinan (2014-01-01)
© 2014 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.The purpose of this study is to develop an accurate and efficient CFD code that can be used in hypersonic flows. The flow analysis is based on the three dimensional Navier-Stokes equations. These equations are solved by using Newton’s method. The analytical method is used to calculate the Jacobian matrix. Flow parameters and convective heat transfer are analyzed on Apollo AS-202 Command Module. Especially, temperature...
Experimental design and statistical modeling methodology for wind tunnel aerodynamics of an agile missile to improve the simulation accuracy and performance
Savas, Ozgun; Topbas, Eren; Unal, Kenan; Karaca, H. Deniz; Kutay, Ali Türker (2018-01-01)
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.Wind tunnel testing is an essential procedure to investigate the aerodynamics forces and moments. In this paper, a methodology is presented to perform such test in an efficient way. Experimental design process is carried out before the testing in order to cover the flight regime as much as possible with the least possible number of tests. After the determination of the test matrix and conducting the wind-on tests, the ...
Analysis and design optimization of three dimensional nozzles
Yildizlar, B.; Eyi, Sinan (2014-01-01)
© 2014 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.The aim of this study is to develop analysis and design optimization method for three dimensional nozzles. For analysis, three dimensional Euler equations are solved using both Newton and Newton-GMRES methods and their performances are compared. The Jacobian matrix needed for Newton method is evaluated analytically. Newton-GMRES method is a matrix free solution technique hence it does not require the Jacobian matrix e...
A Modification to Adaptive Control with Time-varying Learning Rate for Improved Transient Performance
Yayla, Metehan; Kutay, Ali Türker (2022-01-01)
© 2022, American Institute of Aeronautics and Astronautics Inc. All rights reserved.In this study, we propose a new adaptive weight update law using frequency-limited estimation of the matched uncertainty. Many adaptive parameter adjustment laws try to suppress the effects of uncertainties using forcing terms consisting of tracking error only. However, it has been widely studied that including the uncertainty estimation error in the adaptation law enhances the transient performance significantly. In our pro...
Citation Formats
IEEE
ACM
APA
CHICAGO
MLA
BibTeX
M. O. Öztürkmen and Y. Özyörük, “Investigation of a Solution Approach to Quadratic Eigenvalue Problem for Thermoacoustic Instabilities,” presented at the AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022, California, Amerika Birleşik Devletleri, 2022, Accessed: 00, 2022. [Online]. Available: https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85123608792&origin=inward.