{"title":"计算科学与工程促进了对高性能风机和压缩机复杂非定常流动的理解","authors":"S. Gorrell, F. Tsung, Jixian Yao, R. Vickery","doi":"10.1109/HPCMP-UGC.2006.15","DOIUrl":null,"url":null,"abstract":"The ability of high fidelity simulations to more accurately model complex flow phenomena in high performance military fans and compressors is demonstrated. Challenge Project CII continues to investigate how blade row interactions and distortion transfer impact fan and compressor performance. Simulations accomplished through this Challenge Project have produced improved geometric, physical, and numerical fidelity results than previously possible, allowing the design of next generation engines to achieve unprecedented performance","PeriodicalId":173959,"journal":{"name":"2006 HPCMP Users Group Conference (HPCMP-UGC'06)","volume":"11 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2006-06-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"3","resultStr":"{\"title\":\"Computational Science and Engineering Advances Understanding of Complex Unsteady Flows in High Performance Fans and Compressors\",\"authors\":\"S. Gorrell, F. Tsung, Jixian Yao, R. Vickery\",\"doi\":\"10.1109/HPCMP-UGC.2006.15\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The ability of high fidelity simulations to more accurately model complex flow phenomena in high performance military fans and compressors is demonstrated. Challenge Project CII continues to investigate how blade row interactions and distortion transfer impact fan and compressor performance. Simulations accomplished through this Challenge Project have produced improved geometric, physical, and numerical fidelity results than previously possible, allowing the design of next generation engines to achieve unprecedented performance\",\"PeriodicalId\":173959,\"journal\":{\"name\":\"2006 HPCMP Users Group Conference (HPCMP-UGC'06)\",\"volume\":\"11 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2006-06-26\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"3\",\"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.2006.15\",\"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.2006.15","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Computational Science and Engineering Advances Understanding of Complex Unsteady Flows in High Performance Fans and Compressors
The ability of high fidelity simulations to more accurately model complex flow phenomena in high performance military fans and compressors is demonstrated. Challenge Project CII continues to investigate how blade row interactions and distortion transfer impact fan and compressor performance. Simulations accomplished through this Challenge Project have produced improved geometric, physical, and numerical fidelity results than previously possible, allowing the design of next generation engines to achieve unprecedented performance