2011
DOI: 10.1080/13647830.2011.552636
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Investigation of azimuthal staging concepts in annular gas turbines

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Cited by 180 publications
(245 citation statements)
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“…We stress that this statement does not apply to non-symmetric annular combustors, in which the shape function ψ is no longer M-periodic in the azimuthal direction, and in the very specific case where M = 2n in (3.4), where n is the unstable acoustic mode. This latter case is covered by the stability analysis of Noiray et al [7], and shows that mixed modes and standing modes are possible. In this case, the shape function has peaks at the pressure antinodes, and troughs at the pressure nodes of the standing mode.…”
Section: Heat Release Constitutive Equationmentioning
confidence: 99%
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“…We stress that this statement does not apply to non-symmetric annular combustors, in which the shape function ψ is no longer M-periodic in the azimuthal direction, and in the very specific case where M = 2n in (3.4), where n is the unstable acoustic mode. This latter case is covered by the stability analysis of Noiray et al [7], and shows that mixed modes and standing modes are possible. In this case, the shape function has peaks at the pressure antinodes, and troughs at the pressure nodes of the standing mode.…”
Section: Heat Release Constitutive Equationmentioning
confidence: 99%
“…In this representation, the addition of a non-zero asymmetry parameter, C 2n , as proposed in Noiray et al [7], shifts the red point of figure 5 towards one of the A, B axes, maintaining it on the same plane φ ± π/2. Doing so, the system exhibits a superposition of standing and spinning modes.…”
Section: Slow Flowmentioning
confidence: 99%
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