2012
DOI: 10.1016/j.enconman.2011.10.024
|View full text |Cite
|
Sign up to set email alerts
|

Exergetic optimization of a thermoacoustic engine using the particle swarm optimization method

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
9
0
1

Year Published

2013
2013
2020
2020

Publication Types

Select...
8

Relationship

0
8

Authors

Journals

citations
Cited by 28 publications
(12 citation statements)
references
References 24 publications
0
9
0
1
Order By: Relevance
“…Low-emission propulsion/combustion systems are more susceptible to combustion instability. When combustion instability occurs [6][7][8][9][10][11], overheating might occur or the flame may be blow out. Such pressure oscillations may cause structural vibrations and other operational problems.…”
Section: Introductionmentioning
confidence: 99%
“…Low-emission propulsion/combustion systems are more susceptible to combustion instability. When combustion instability occurs [6][7][8][9][10][11], overheating might occur or the flame may be blow out. Such pressure oscillations may cause structural vibrations and other operational problems.…”
Section: Introductionmentioning
confidence: 99%
“…These oscillations are mainly caused by the http://dx.doi.org/10.1016/j.apenergy.2015.04.026 0306-2619/Ó 2015 Elsevier Ltd. All rights reserved. energy transferred from the heat source to sound waves [10][11][12][13][14][15][16][17], which depends upon the nature of coupling between the flame and oncoming flow fluctuations [18,19]. Small amplitude flow disturbances can excite natural modes of combustion chamber and cause them to grow into a nonlinear limit cycle.…”
Section: Introductionmentioning
confidence: 98%
“…Step 3 On the basis of the adaptive degree, the so-far best position pbest for each particle, the so-far best position for the entire swarm gbest are calculated and the new particles will be generated using Equations (14-18) mentioned above and Equation (19), Equation (19) is expressed as follows: (19) where d = 1, 2,…., D − 1, i = 1, 2,…., N, t = 1, 2,…., t max , and satisfies the following restrictions: (20) Step 4 Check whether the termination criteria are satisfied. The termination criteria are either achieving the forecasting precision or reaching the maximum iteration number.…”
Section: Determination Of Weight Coefficients By Epso Algorithmmentioning
confidence: 99%
“…The PSO algorithm is considered an effective tool for solving engineering optimization problems for ordinary differential equations [19]. Each individual in the PSO flies in the search space with a velocity which is dynamically adjusted according to its own flying experience and flying experience of its companions [20]. In a PSO system, each particle saves its own best position and also saves the best position found so far in the search-space by which all the swarm is expected to move toward it [21].…”
Section: Principle Of Epso Algorithmmentioning
confidence: 99%