T. Arakawa, Kiyoshi Nojima, Kan Kobayashi, S. Tomioka
{"title":"双模燃烧室中反应流和非反应流中的燃料/空气混合","authors":"T. Arakawa, Kiyoshi Nojima, Kan Kobayashi, S. Tomioka","doi":"10.2322/TJSASS.64.71","DOIUrl":null,"url":null,"abstract":"An experimental investigation on fuel and air mixing characteristics within a dual-mode combustor is presented. To determine the dominant parameters of mixing characteristics of fuel with air fl ow, fuel (H 2 or C 2 H 4 ) or inert gas (He, N 2 or Ar) were perpendicularity injected from plural circular ori fi ces into high- or room-temperature M2.5 air fl ows decelerated through pseudo-shockwave systems. Under similar dynamic pressure ratios, fuel mass fl ux contours downstream of the injector were similar between the H 2 and C 2 H 4 reacting cases. However, fuel mass fl ux contours were di ff erent between the C 2 H 4 reacting and Ar non-reacting cases due to the heat-release e ff ect during local mixing. On the other hand, heat-release e ff ect on mixing e ffi ciency was found to be minor in bulk-scale mixing evaluation. It was found that C 2 H 4 mixing e ffi ciency with an equivalence ratio of 1.6 could be predicted within an error of a few percent from Ar mixing results under similar dynamic pressure ratio and similar peak pressure.","PeriodicalId":54419,"journal":{"name":"Transactions of the Japan Society for Aeronautical and Space Sciences","volume":"1 1","pages":""},"PeriodicalIF":0.7000,"publicationDate":"2021-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Fuel/Air Mixing in Reacting and Non-reacting Flows within a Dual-mode Combustor\",\"authors\":\"T. Arakawa, Kiyoshi Nojima, Kan Kobayashi, S. Tomioka\",\"doi\":\"10.2322/TJSASS.64.71\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"An experimental investigation on fuel and air mixing characteristics within a dual-mode combustor is presented. To determine the dominant parameters of mixing characteristics of fuel with air fl ow, fuel (H 2 or C 2 H 4 ) or inert gas (He, N 2 or Ar) were perpendicularity injected from plural circular ori fi ces into high- or room-temperature M2.5 air fl ows decelerated through pseudo-shockwave systems. Under similar dynamic pressure ratios, fuel mass fl ux contours downstream of the injector were similar between the H 2 and C 2 H 4 reacting cases. However, fuel mass fl ux contours were di ff erent between the C 2 H 4 reacting and Ar non-reacting cases due to the heat-release e ff ect during local mixing. On the other hand, heat-release e ff ect on mixing e ffi ciency was found to be minor in bulk-scale mixing evaluation. It was found that C 2 H 4 mixing e ffi ciency with an equivalence ratio of 1.6 could be predicted within an error of a few percent from Ar mixing results under similar dynamic pressure ratio and similar peak pressure.\",\"PeriodicalId\":54419,\"journal\":{\"name\":\"Transactions of the Japan Society for Aeronautical and Space Sciences\",\"volume\":\"1 1\",\"pages\":\"\"},\"PeriodicalIF\":0.7000,\"publicationDate\":\"2021-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Transactions of the Japan Society for Aeronautical and Space Sciences\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://doi.org/10.2322/TJSASS.64.71\",\"RegionNum\":4,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q4\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Transactions of the Japan Society for Aeronautical and Space Sciences","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.2322/TJSASS.64.71","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
Fuel/Air Mixing in Reacting and Non-reacting Flows within a Dual-mode Combustor
An experimental investigation on fuel and air mixing characteristics within a dual-mode combustor is presented. To determine the dominant parameters of mixing characteristics of fuel with air fl ow, fuel (H 2 or C 2 H 4 ) or inert gas (He, N 2 or Ar) were perpendicularity injected from plural circular ori fi ces into high- or room-temperature M2.5 air fl ows decelerated through pseudo-shockwave systems. Under similar dynamic pressure ratios, fuel mass fl ux contours downstream of the injector were similar between the H 2 and C 2 H 4 reacting cases. However, fuel mass fl ux contours were di ff erent between the C 2 H 4 reacting and Ar non-reacting cases due to the heat-release e ff ect during local mixing. On the other hand, heat-release e ff ect on mixing e ffi ciency was found to be minor in bulk-scale mixing evaluation. It was found that C 2 H 4 mixing e ffi ciency with an equivalence ratio of 1.6 could be predicted within an error of a few percent from Ar mixing results under similar dynamic pressure ratio and similar peak pressure.