SHAPE OPTIMIZATION OF THERMOACOUSTIC SYSTEMS USING A 2D ADJOINT HELMHOLTZ SOLVER

被引:0
作者
Falco, Stefano [1 ]
Juniper, Matthew P. [1 ]
机构
[1] Univ Cambridge, Dept Engn, Cambridge CB2 1PZ, England
来源
PROCEEDINGS OF THE ASME TURBO EXPO 2020: TURBOMACHINERY TECHNICAL CONFERENCE AND EXHIBITION, VOL 4A | 2020年
基金
欧盟地平线“2020”;
关键词
FLAME DESCRIBING FUNCTION; SENSITIVITY-ANALYSIS; COMBUSTION INSTABILITY; STABILITY;
D O I
暂无
中图分类号
O414.1 [热力学];
学科分类号
摘要
Thermoacoustic instabilities, which arise due to the interaction between flames and acoustics, are sensitive to small changes to the system parameters. In this paper, we apply adjoint-based shape optimization to a 2D finite element Helmholtz solver to find accurately and inexpensively the shape changes that most stabilise a 2D thermoacoustic system in the linear regime. We examine two cases: a Rijke tube and a turbulent swirl combustor. Both systems exhibit an unstable longitudinal mode and we suppress the instability by slightly modifying the geometry. In the case of the turbulent swirl combustor, the sensitivities are higher in the plenum and in the burner than in the combustion chamber, mainly due to the effect of the mean temperature. In the cooler regions, the local wavelength is shorter, which means that geometry changes of a given distance have more influence than they do where the local wavelength is longer. This is the first time adjoint-based shape optimization is applied to 2D Helmholtz solvers in thermoacoustics, after being previously applied to low-order thermoacoustic networks. But Helmholtz solvers have an intrinsic advantage: they can handle complex geometries. The easy scalability of this method to complex 3D geometries make this tool a strong candidate for the iterative design of thermoacoustically stable combustors.
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页数:10
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共 38 条
[1]  
Aguilar JG, 2018, PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 4A
[2]   Adjoint-based sensitivity analysis of low-order thermoacoustic networks using a wave-based approach [J].
Aguilar, Jose G. ;
Magri, Luca ;
Juniper, Matthew P. .
JOURNAL OF COMPUTATIONAL PHYSICS, 2017, 341 :163-181
[3]  
Alnaes M, 2015, ARCH NUMER SOFTW, V3, DOI DOI 10.11588/ANS.2015.100.20553
[4]  
[Anonymous], 2014, P CENT TURB RES SUMM
[5]   Thermoacoustic analysis of a laminar premixed flame using a linearized reactive flow solver [J].
Avdonin, Alexander ;
Meindl, Max ;
Polifke, Wolfgang .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 37 (04) :5307-5314
[6]   Uncertainty quantification and sensitivity analysis of thermoacoustic stability with non-intrusive polynomial chaos expansion [J].
Avdonin, Alexander ;
Jaensch, Stefan ;
Silva, Camilo F. ;
Cesnovar, Matic ;
Polifke, Wolfgang .
COMBUSTION AND FLAME, 2018, 189 :300-310
[7]   Shape sensitivity of eigenvalues in hydrodynamic stability, with physical interpretation for the flow around a cylinder [J].
Brewster, Jack ;
Juniper, Matthew P. .
EUROPEAN JOURNAL OF MECHANICS B-FLUIDS, 2020, 80 :80-91
[8]  
Chu B.T., 1965, Acta Mech., V1, P215
[9]   ASPECTS OF COMBUSTION STABILITY IN LIQUID PROPELLANT ROCKET MOTORS .1. FUNDAMENTALS - LOW FREQUENCY INSTABILITY WITH MONOPROPELLANTS [J].
CROCCO, L .
JOURNAL OF THE AMERICAN ROCKET SOCIETY, 1951, 21 (06) :163-178
[10]  
Delfour M, 2011, ADV DES CONTROL, pXIX, DOI 10.1137/1.9780898719826