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Cited by 10 publications
(8 citation statements)
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“…13 This projection method relies on Hodge decomposition of the intermediate velocity field U * as. 15…”
Section: Basic Model and Numerical Methodsmentioning
confidence: 99%
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“…13 This projection method relies on Hodge decomposition of the intermediate velocity field U * as. 15…”
Section: Basic Model and Numerical Methodsmentioning
confidence: 99%
“…In other words, the target information can always be captured. The influences of this motion along X-axis, Y-axis and Z-axis on the azimuth and pitch angles can be described as equations (15) to (17):…”
Section: Perturbation Solution Of the Azimuth/pitch Anglesmentioning
confidence: 99%
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“…However, the high energy content of the combustion showed that the mesh quality near the walls can be coarser than it is required in the case of channel flows. It should be noted that the k-ε model has failed to provide a realistic inlet flow, however, it is usually acceptable for modeling the turbulent viscosity in combustion chamber geometries in which volumetric processes dominate [19].…”
Section: Methodsmentioning
confidence: 99%
“…This contribution can be split into a first part due to velocity fluctuations V false^ and a second one due to the turbulent flame speed fluctuations U ^ t which can be expressed in terms of fuel mixture fraction fluctuations on the basis of relation (18). Regarding the first part, the velocity fluctuation orthogonal to the flame V false^ was decomposed in 13 into an irrotational V ^ i and a rotational V false^ r contributions using the Helmholtz-Hodge decomposition. 14 The irrotational velocity part V ^ i is due to the pure acoustic perturbation which is characterized by wavelength much longer than the flame length, i.e.…”
Section: Linearizationmentioning
confidence: 99%