{"title":"On the effects of non-zero yaw on leading-edge tubercled wings","authors":"T. H. New, S. Mandrà","doi":"10.1186/s42774-024-00182-4","DOIUrl":null,"url":null,"abstract":"Steady-state numerical simulations were conducted to capture the aerodynamic characteristics and flow patterns resulting from a tubercled and non-tubercled wing subjected to various combined pitch and yaw conditions at $$Re=1.8 \\times 10^{5}$$ . Pitch angle ranged from $$0^{\\circ }$$ to $$25^{\\circ }$$ , while two different yaw angles of $$10^{\\circ }$$ and $$30^{\\circ }$$ were used. Results show that $$10^{\\circ }$$ yaw angle does not impact upon the lift and drag characteristics significantly, while a $$30^{\\circ }$$ yaw angle leads to substantial lift and drag losses. Additionally, the tubercled wing continues to confer favourable stall-mitigating characteristics even for the larger yaw angle. Finally, despite skewing the flow structures significantly, the $$30^{\\circ }$$ yaw angle also reduces the formations of bi-periodic flow structures, flow separations and recirculating regions along the leading-edge tubercles, suggesting potentially better flow stability and controllability. • Steady-state numerical study is conducted on NACA 634021 baseline and tubercled wings • Two yaw angles of $$10^{\\circ }$$ and $$30^{\\circ }$$ are used together with pitch angles from $$0^{\\circ }$$ to $$25^{\\circ }$$ • Results show $$10^{\\circ }$$ yaw angle has minimal impact on the lift and drag characteristics, while $$30^{\\circ }$$ yaw angle reduces both lift and drag levels significantly • Larger yaw angle leads to more skewed flows, as well as reduced flow separations and recirculating regions • Larger yaw angle also suppresses bi-periodic flow behaviour in tubercled wings, suggesting better flow stability and controllability","PeriodicalId":33737,"journal":{"name":"Advances in Aerodynamics","volume":null,"pages":null},"PeriodicalIF":2.9000,"publicationDate":"2024-09-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Advances in Aerodynamics","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.1186/s42774-024-00182-4","RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
引用次数: 0
Abstract
Steady-state numerical simulations were conducted to capture the aerodynamic characteristics and flow patterns resulting from a tubercled and non-tubercled wing subjected to various combined pitch and yaw conditions at $$Re=1.8 \times 10^{5}$$ . Pitch angle ranged from $$0^{\circ }$$ to $$25^{\circ }$$ , while two different yaw angles of $$10^{\circ }$$ and $$30^{\circ }$$ were used. Results show that $$10^{\circ }$$ yaw angle does not impact upon the lift and drag characteristics significantly, while a $$30^{\circ }$$ yaw angle leads to substantial lift and drag losses. Additionally, the tubercled wing continues to confer favourable stall-mitigating characteristics even for the larger yaw angle. Finally, despite skewing the flow structures significantly, the $$30^{\circ }$$ yaw angle also reduces the formations of bi-periodic flow structures, flow separations and recirculating regions along the leading-edge tubercles, suggesting potentially better flow stability and controllability. • Steady-state numerical study is conducted on NACA 634021 baseline and tubercled wings • Two yaw angles of $$10^{\circ }$$ and $$30^{\circ }$$ are used together with pitch angles from $$0^{\circ }$$ to $$25^{\circ }$$ • Results show $$10^{\circ }$$ yaw angle has minimal impact on the lift and drag characteristics, while $$30^{\circ }$$ yaw angle reduces both lift and drag levels significantly • Larger yaw angle leads to more skewed flows, as well as reduced flow separations and recirculating regions • Larger yaw angle also suppresses bi-periodic flow behaviour in tubercled wings, suggesting better flow stability and controllability