Unsteady flow simulation of leading-edge separation in thinairfoil cascade

A modification to turbulence model

Atsushi Tateishi, Toshinori Watanabe, Takehiro Himeno, Chihiro Inoue

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Leading edge separation of thin airfoil cascade in subsonic flow at large angle of incidence was simulated by implicit large eddy simulation (ILES) and Reynolds averaged Navier-Stokes (RANS) simulations with various turbulence models. In the ILES simulations with fine grids, the timeaveraged surface pressure qualitatively agreed with the experimental data. The RANS and ILES simulations on the coarse mesh failed to capture a peak of pressure near the leading edge. From spectrum analysis, it was observed that the flow-field was turbulent in the separation bubble. In the failed RANS simulations, the separation bubble was much longer and the turbulence energy near the leading edge was much lower than those in the ILES results. The development of lambdashaped vortex structures and their sudden weakening near the reattachment point was observed in the unsteady simulations. Two possible modifications to existing turbulence models in RANS simulations were proposed based on the comparison of turbulence energy between the ILES and RANS results. It is shown that these modifications improve the bubble length and Cp distributions of RANS simulations, though further validation and modeling are needed for the application to realistic cases.

Original languageEnglish
Title of host publicationTurbomachinery
PublisherAmerican Society of Mechanical Engineers (ASME)
ISBN (Electronic)9780791856642, 9780791856642
DOIs
Publication statusPublished - Jan 1 2015
EventASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015 - Montreal, Canada
Duration: Jun 15 2015Jun 19 2015

Publication series

NameProceedings of the ASME Turbo Expo
Volume2B

Other

OtherASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015
CountryCanada
CityMontreal
Period6/15/156/19/15

Fingerprint

Flow simulation
Large eddy simulation
Unsteady flow
Turbulence models
Turbulence
Subsonic flow
Cascades (fluid mechanics)
Airfoils
Spectrum analysis
Flow fields
Vortex flow

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Tateishi, A., Watanabe, T., Himeno, T., & Inoue, C. (2015). Unsteady flow simulation of leading-edge separation in thinairfoil cascade: A modification to turbulence model. In Turbomachinery (Proceedings of the ASME Turbo Expo; Vol. 2B). American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/GT201543849

Unsteady flow simulation of leading-edge separation in thinairfoil cascade : A modification to turbulence model. / Tateishi, Atsushi; Watanabe, Toshinori; Himeno, Takehiro; Inoue, Chihiro.

Turbomachinery. American Society of Mechanical Engineers (ASME), 2015. (Proceedings of the ASME Turbo Expo; Vol. 2B).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Tateishi, A, Watanabe, T, Himeno, T & Inoue, C 2015, Unsteady flow simulation of leading-edge separation in thinairfoil cascade: A modification to turbulence model. in Turbomachinery. Proceedings of the ASME Turbo Expo, vol. 2B, American Society of Mechanical Engineers (ASME), ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015, Montreal, Canada, 6/15/15. https://doi.org/10.1115/GT201543849
Tateishi A, Watanabe T, Himeno T, Inoue C. Unsteady flow simulation of leading-edge separation in thinairfoil cascade: A modification to turbulence model. In Turbomachinery. American Society of Mechanical Engineers (ASME). 2015. (Proceedings of the ASME Turbo Expo). https://doi.org/10.1115/GT201543849
Tateishi, Atsushi ; Watanabe, Toshinori ; Himeno, Takehiro ; Inoue, Chihiro. / Unsteady flow simulation of leading-edge separation in thinairfoil cascade : A modification to turbulence model. Turbomachinery. American Society of Mechanical Engineers (ASME), 2015. (Proceedings of the ASME Turbo Expo).
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