{"title":"Cray X1旋翼机CFD准定常涡跟踪","authors":"YikLoon Lee","doi":"10.1109/HPCMP-UGC.2006.62","DOIUrl":null,"url":null,"abstract":"High-fidelity, far-field and economical blade vortex capturing, tracking and subsequent interaction is one of the most important aerodynamics problems in rotorcraft, particularly for heavy lift. Its solution is also one of the most difficult to obtain. This paper documents the use of multiple helical vortex tracking grids and development of an automated tracking technique to achieve this objective. This technique is tested on the interactional aerodynamics of a generic quad tilt rotor (QTR). This paper also highlights the special issues that arise in the parallelization of an in-house overset CFD code using the one-sided communication model of Co-Array Fortran (CAF) implemented on the Cray XIE","PeriodicalId":173959,"journal":{"name":"2006 HPCMP Users Group Conference (HPCMP-UGC'06)","volume":"122 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2006-06-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Quasi-Steady Vortex Tracking in Rotorcraft CFD on the Cray X1\",\"authors\":\"YikLoon Lee\",\"doi\":\"10.1109/HPCMP-UGC.2006.62\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"High-fidelity, far-field and economical blade vortex capturing, tracking and subsequent interaction is one of the most important aerodynamics problems in rotorcraft, particularly for heavy lift. Its solution is also one of the most difficult to obtain. This paper documents the use of multiple helical vortex tracking grids and development of an automated tracking technique to achieve this objective. This technique is tested on the interactional aerodynamics of a generic quad tilt rotor (QTR). This paper also highlights the special issues that arise in the parallelization of an in-house overset CFD code using the one-sided communication model of Co-Array Fortran (CAF) implemented on the Cray XIE\",\"PeriodicalId\":173959,\"journal\":{\"name\":\"2006 HPCMP Users Group Conference (HPCMP-UGC'06)\",\"volume\":\"122 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2006-06-26\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2006 HPCMP Users Group Conference (HPCMP-UGC'06)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/HPCMP-UGC.2006.62\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2006 HPCMP Users Group Conference (HPCMP-UGC'06)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/HPCMP-UGC.2006.62","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Quasi-Steady Vortex Tracking in Rotorcraft CFD on the Cray X1
High-fidelity, far-field and economical blade vortex capturing, tracking and subsequent interaction is one of the most important aerodynamics problems in rotorcraft, particularly for heavy lift. Its solution is also one of the most difficult to obtain. This paper documents the use of multiple helical vortex tracking grids and development of an automated tracking technique to achieve this objective. This technique is tested on the interactional aerodynamics of a generic quad tilt rotor (QTR). This paper also highlights the special issues that arise in the parallelization of an in-house overset CFD code using the one-sided communication model of Co-Array Fortran (CAF) implemented on the Cray XIE