The influence of the blade tip shape on brownout by an approach based on computational fluid dynamics. Issue 1 (1st January 2021)
- Record Type:
- Journal Article
- Title:
- The influence of the blade tip shape on brownout by an approach based on computational fluid dynamics. Issue 1 (1st January 2021)
- Main Title:
- The influence of the blade tip shape on brownout by an approach based on computational fluid dynamics
- Authors:
- Hu, Jianping
Xu, Guohua
Shi, Yongjie
Huang, Shuilin - Abstract:
- Abstract : In this study, a computational fluid dynamics approach based on solving the Reynolds-averaged Navier-Stokes equation and shear stress transport (SST) (Menter) k-ω turbulence model is used to solve the rotor in ground effect. A discrete element method based on solving the Hertz-Mindlin (no-slip) contact model and considering the real physical properties and collision is used to solve the motion and distribution of sediment particles in the field. By coupling the two approaches, the dust cloud development in the ground-effect flow field of a helicopter with rectangular-tip and slotted-tip blades is simulated for six seconds. The characteristics of the flow field are analyzed, and the influence of the flow field generated by the two types of blades on the movement and distribution of sediment particles on the ground and the subsequent dust cloud development over time are compared. The relatively long time of numerical results show that the sediment particles initially located on the ground are uplifted by the interaction between the blade tip vortex and the ground. Over time, the particles become more concentrated around the tip vortex core. The sediment particles in the dust cloud move primarily in the radial and axial directions of the rotation center, and the circumferential movement is not significant. The optimized slotted-tip blade provides better dissipation of the tip vortex core intensity near the ground than the rectangular-tip blade, thus weakening theAbstract : In this study, a computational fluid dynamics approach based on solving the Reynolds-averaged Navier-Stokes equation and shear stress transport (SST) (Menter) k-ω turbulence model is used to solve the rotor in ground effect. A discrete element method based on solving the Hertz-Mindlin (no-slip) contact model and considering the real physical properties and collision is used to solve the motion and distribution of sediment particles in the field. By coupling the two approaches, the dust cloud development in the ground-effect flow field of a helicopter with rectangular-tip and slotted-tip blades is simulated for six seconds. The characteristics of the flow field are analyzed, and the influence of the flow field generated by the two types of blades on the movement and distribution of sediment particles on the ground and the subsequent dust cloud development over time are compared. The relatively long time of numerical results show that the sediment particles initially located on the ground are uplifted by the interaction between the blade tip vortex and the ground. Over time, the particles become more concentrated around the tip vortex core. The sediment particles in the dust cloud move primarily in the radial and axial directions of the rotation center, and the circumferential movement is not significant. The optimized slotted-tip blade provides better dissipation of the tip vortex core intensity near the ground than the rectangular-tip blade, thus weakening the entrainment effect of the sediment particles on the ground and reducing the dust cloud concentration around the disc plane. … (more)
- Is Part Of:
- Engineering applications of computational fluid mechanics. Volume 15:Issue 1(2021)
- Journal:
- Engineering applications of computational fluid mechanics
- Issue:
- Volume 15:Issue 1(2021)
- Issue Display:
- Volume 15, Issue 1 (2021)
- Year:
- 2021
- Volume:
- 15
- Issue:
- 1
- Issue Sort Value:
- 2021-0015-0001-0000
- Page Start:
- 692
- Page End:
- 711
- Publication Date:
- 2021-01-01
- Subjects:
- In-ground-effect -- brownout -- CFD -- DEM -- coupling
Computational fluid dynamics -- Periodicals
620.10640285 - Journal URLs:
- http://www.tandfonline.com/toc/tcfm20/current ↗
http://www.tandfonline.com/ ↗ - DOI:
- 10.1080/19942060.2021.1917454 ↗
- Languages:
- English
- ISSNs:
- 1994-2060
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 25381.xml