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Published September 2020 | Version v1
Journal article

The effect of bend angle on pressure drop and flow behavior in a corrugated duct

  • 1. Shanghai Key Lab of Vehicle Aerodynamics and Vehicle Thermal Management Systems (China)
  • 2. Tongji University. Shanghai Automotive Wind Tunnel Center (China)
  • 3. Tongji University. School of Aerospace Engineering and Applied Mechanics (China)
  • 4. Beijing Aeronautical Science and Technology Research Institute (China)
  • 5. Boeing Research & Technology - China (China)
  • 6. Boeing Commercial Airplanes (United States)
  • 7. China Aerodynamics Research and Development Center. Key Laboratory of Icing and Anti/De-icing of Aircraft (China)

Description

In the present study, the effect of bend angle on pressure drop and flow behavior in a small-diameter corrugated duct is numerically investigated and experimentally validated under a fully developed flow condition. The large eddy simulation, together with the proper orthogonal decomposition (POD) method, is employed to study the pressure drop, mean flow pattern, and unsteady flow evolution for a corrugated duct with various bend angles. The results show that the pressure drop exhibits a monotonic increase with increasing bend angle. Specifically, as the bend angle increases from 0 to 90, the pressure drop of the corrugated duct experiences a striking increase of about 43%. Accordingly, a larger bend angle is found to induce the occurrence of stronger Dean cells or larger swirl intensity downstream the duct bend. Meanwhile, as for larger bend angles, the main turbulent properties of the Dean cells could be, to some extent, governed by the first few POD modes, which appear to be featured with one or a few large-scale vortices. Generally, the larger bend angle causes stronger swirl intensity and wave-like structures, thus rendering severer pressure drop or larger pressure loss coefficient in the corrugated duct.

Additional details

Identifiers

Publishing Information

Journal Title
Acta Mechanica
Journal Volume
231
Journal Issue
9
Journal Page Range
p. 3755-3777
ISSN
0001-5970
CODEN
AMHCAP

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Copyright
Copyright (c) 2020 © Springer-Verlag GmbH Austria, part of Springer Nature 2020