The response mechanism of pressure fluctuation to the unsteady heat release in a strong rotating environment
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Published version
Author(s)
Ren, Shoujun
Tian, Bo
Jones, William P
Wang, Xiaohan
Type
Journal Article
Abstract
The response mechanism of the pressure fluctuation to the unsteady heat release rate at the ‘unsteady’ combustion state in a strong rotating environment was investigated using a stratified vortex-tube combustor via a large eddy simulation method. Results show that the peak amplitude of heat release fluctuation at the ‘unsteady’ state is just 2.8 × 106 W/m3 and the peak amplitude of pressure fluctuation is always within 3000 Pa based on the vortex-tube configuration, indicating a weak fluctuation degree. The unsteady heat release does not bring about a higher momentum flux fluctuation due to quick momentum damping in the rotating reactive environment. The pressure fluctuation does not relate closely to the momentum flux and its fluctuation; this is due to the effect of the centrifugal force caused by rotating behavior. After splitting the momentum flux into the different components, we found that the tangential component acts in reverse to that of the radial and axial directions in the exterior region. Viz., the pressure increases when the tangential momentum flux increases in the exterior region but decreases when the radial and axial components increase. The laminarization of the fluid suppresses the fluctuations in the radial and axial directions only, therefore the uneven attenuation of the momentum flux fluctuation in different directions is the dominant cause of the enlarged pressure fluctuation in the ‘unsteady’ burning state. Moreover, we find that the pressure fluctuation degree is also closely related to the centrifugal weight coefficient. When this coefficient is far away from zero, the centrifugal effect will become obvious, and vice versa.
Date Issued
2023-08
Date Acceptance
2023-04-19
Citation
Aerospace Science and Technology, 2023, 139
ISSN
1270-9638
Publisher
Elsevier
Journal / Book Title
Aerospace Science and Technology
Volume
139
Copyright Statement
© 2023 The Authors. Published by Elsevier Masson SAS. This is an open access article under the CC BY-NC-ND license
Identifier
https://www.webofscience.com/api/gateway?GWVersion=2&SrcApp=PARTNER_APP&SrcAuth=LinksAMR&KeyUT=WOS:001001275200001&DestLinkType=FullRecord&DestApp=ALL_WOS&UsrCustomerID=a2bf6146997ec60c407a63945d4e92bb
Subjects
Centrifugal weight coefficient
COMBUSTION
Engineering
Engineering, Aerospace
FLAMES
FLOWS
LARGE-EDDY SIMULATION
Momentum flux
PROBABILITY DENSITY-FUNCTION
Response mechanism
SCALAR
Science & Technology
Technology
Uneven attenuation
Vortex -tube combustor
Publication Status
Published
Article Number
ARTN 108356
Date Publish Online
2023-05-02