Influence of non-iterative time-advancement schemes on the aerodynamic prediction of pitching airfoils using dynamic mesh

Abdessemed, Chawki; Yao, Yufeng; Bouferrouk, Abdessalem; Narayan, Pritesh

Abstract

A pitching airfoil problem is addressed in this paper to assess the use of a non-iterative time-advancement (NITA) scheme with dynamic mesh method, and also to estimate possible CPU time savings. Simulations have shown that using a combination of dynamic mesh and NITA scheme can efficiently predict dynamic loads with quality results similar to those obtained by iterative time-advancement scheme and sliding mesh method, but merely consuming half of CPU time of the latter approach. This study also confirms the validity of an in-house developed user-defined function integrated in a RANS CFD solver and demonstrates the efficiency and the accuracy of NITA scheme.

Citation

Abdessemed, C., Yao, Y., Bouferrouk, A., & Narayan, P. (2019, June). Influence of non-iterative time-advancement schemes on the aerodynamic prediction of pitching airfoils using dynamic mesh. Paper presented at 8th International Symposium on Physics of Fluids (ISPF8), Xian, China

• Presentation Conference Type: Conference Paper (unpublished)
• Conference Name: 8th International Symposium on Physics of Fluids (ISPF8)
• Conference Location: Xian, China
• Start Date: Jun 10, 2019
• End Date: Jun 13, 2019
• Acceptance Date: Apr 1, 2019
• Peer Reviewed: Not Peer Reviewed
• Keywords: dynamic mesh, CFD, RANS, NITA, pitching airfoil, time-advancement scheme
• Public URL: https://uwe-repository.worktribe.com/output/1493684
• Additional Information: Title of Conference or Conference Proceedings : 8th International Symposium on Physics of Fluids (ISPF8) 10-13 June, 2019, Xian, China