A COMPUTATIONAL STUDY ON BLADE-VORTEX INTERACTION FOR COAXIAL ROTORS IN HOVER USING A NOVEL HIGH-ORDER SCHEME

Shaoqiang Han, Wenping Song, Zhonghua Han

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

1 Scopus citations

Abstract

Accurate prediction of tip vortices is crucial for mechanism study on the blade-vortex interaction(BVI) for coaxial rotors. A new high-order scheme (WENO-K) proposed by our research group is employed to minimize numerical dissipation and extended to numerical simulation of unsteady flows dominated by tip vortices around hovering coaxial rotors. WENO-K is referred to as an adaptively optimized WENO scheme with Gauss-Kriging reconstruction, and its advantage is to reduce dissipation in smooth regions of flow while preserving high-resolution around discontinuities. Here WENO-K scheme is adopted to reconstruct left and right state values within the Roe Riemann solver updating the inviscid fluxes on a structured dynamic overset grid. To minimize the accuracy loss for high-order reconstruction on artificial boundaries of overset grid, a method of multilayer fringes is proposed to carry out interpolation between background grid and blade grid. A conservative method is developed for the flow variable interpolation in the overset grid interface. High-accurate numerical simulation of vortex wake structure over a coaxial rotor was carried out. The results indicates that the tip vortex structure and its unsteady generation, development and evolution process can be completely simulated and preserved by WENO-K scheme, and the pressure impulses on the blade caused by BVI can also be well captured.

Original languageEnglish
Title of host publication33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022
PublisherInternational Council of the Aeronautical Sciences
Pages1985-1998
Number of pages14
ISBN (Electronic)9781713871163
StatePublished - 2022
Event33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022 - Stockholm, Sweden
Duration: 4 Sep 20229 Sep 2022

Publication series

Name33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022
Volume3

Conference

Conference33rd Congress of the International Council of the Aeronautical Sciences, ICAS 2022
Country/TerritorySweden
CityStockholm
Period4/09/229/09/22

Keywords

  • blade-tip vortex
  • blade-vortex interaction
  • Coaxial rotor
  • high-order scheme
  • unsteady flow

Fingerprint

Dive into the research topics of 'A COMPUTATIONAL STUDY ON BLADE-VORTEX INTERACTION FOR COAXIAL ROTORS IN HOVER USING A NOVEL HIGH-ORDER SCHEME'. Together they form a unique fingerprint.

Cite this