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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2019
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Article
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Fig 7
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Research Article
Thermoacoustic Stability Boundaries in the Model Combustion Chamber with a Gas-Centered Swirl Coaxial Injector
Figure 7
Damping factors for various test conditions in (a) set no. 3 and (b) set no. 4.
(a)
Set no. 3
(b)
Set no. 4