Jingying Zuo , Jingjia Xue , Silong Zhang , Jianfei Wei , Xin Li , Wen Bao , Naigang Cui
{"title":"以气态烃类燃料为冷却剂的分段喷射调节超声速气膜冷却研究","authors":"Jingying Zuo , Jingjia Xue , Silong Zhang , Jianfei Wei , Xin Li , Wen Bao , Naigang Cui","doi":"10.1016/j.ijthermalsci.2025.110281","DOIUrl":null,"url":null,"abstract":"<div><div>Hydrocarbon fueled supersonic film cooling is considered to be one of the most promising thermal protection methods for scramjet combustors, while regulating its flow and combustion characteristics and improving its cooling performance are of great significance for engine performance. In this paper, the effects of segmented injection regulation method on hydrocarbon fueled supersonic film cooling performance are numerically investigated. The results indicate that, with single film injection, film combustion first brings beneficial effect and then brings negative effect on the supersonic film cooling. Whereas, segmented injection reorganizes near-wall chemical reaction and flow characteristics, resulting in endothermic-exothermic- endothermic reaction characteristics near the wall, leading to the combustion high-temperature region distributed in the film potential-core flow characteristic region and suppressing the mixing process. Therefore, segmented injection regulation method can significantly shorten the negative effect region brought by the film combustion, and further improve the supersonic film cooling performance based on that with single film injection. It is worth mentioning that, the overall film cooling performance with segmented injection is not sensitive to the flow distribution ratio in the variation range from 5:5 to 7:3. Furthermore, the second film injection arranges at the separation point of the first film, where the combustion begins to have negative effect on the film cooling, can eliminate the negative effect. Within the 500 mm length range without increasing the mass flow rate of film coolant, segmented injection by dual films with flow equalization principle and evenly distributed position can increase the average supersonic film cooling effectiveness by 19 %, and decrease the average wall skin friction by 20.1 %. The forward movement of the second film layout position to the separation point can further increase the average supersonic film cooling effectiveness by 2.85 %.</div></div>","PeriodicalId":341,"journal":{"name":"International Journal of Thermal Sciences","volume":"220 ","pages":"Article 110281"},"PeriodicalIF":5.0000,"publicationDate":"2025-09-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Study on supersonic film cooling using gaseous hydrocarbon fuel as coolant with segmented injection regulation method\",\"authors\":\"Jingying Zuo , Jingjia Xue , Silong Zhang , Jianfei Wei , Xin Li , Wen Bao , Naigang Cui\",\"doi\":\"10.1016/j.ijthermalsci.2025.110281\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Hydrocarbon fueled supersonic film cooling is considered to be one of the most promising thermal protection methods for scramjet combustors, while regulating its flow and combustion characteristics and improving its cooling performance are of great significance for engine performance. In this paper, the effects of segmented injection regulation method on hydrocarbon fueled supersonic film cooling performance are numerically investigated. The results indicate that, with single film injection, film combustion first brings beneficial effect and then brings negative effect on the supersonic film cooling. Whereas, segmented injection reorganizes near-wall chemical reaction and flow characteristics, resulting in endothermic-exothermic- endothermic reaction characteristics near the wall, leading to the combustion high-temperature region distributed in the film potential-core flow characteristic region and suppressing the mixing process. Therefore, segmented injection regulation method can significantly shorten the negative effect region brought by the film combustion, and further improve the supersonic film cooling performance based on that with single film injection. It is worth mentioning that, the overall film cooling performance with segmented injection is not sensitive to the flow distribution ratio in the variation range from 5:5 to 7:3. Furthermore, the second film injection arranges at the separation point of the first film, where the combustion begins to have negative effect on the film cooling, can eliminate the negative effect. Within the 500 mm length range without increasing the mass flow rate of film coolant, segmented injection by dual films with flow equalization principle and evenly distributed position can increase the average supersonic film cooling effectiveness by 19 %, and decrease the average wall skin friction by 20.1 %. The forward movement of the second film layout position to the separation point can further increase the average supersonic film cooling effectiveness by 2.85 %.</div></div>\",\"PeriodicalId\":341,\"journal\":{\"name\":\"International Journal of Thermal Sciences\",\"volume\":\"220 \",\"pages\":\"Article 110281\"},\"PeriodicalIF\":5.0000,\"publicationDate\":\"2025-09-06\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"International Journal of Thermal Sciences\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1290072925006040\",\"RegionNum\":2,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, MECHANICAL\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Thermal Sciences","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1290072925006040","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
Study on supersonic film cooling using gaseous hydrocarbon fuel as coolant with segmented injection regulation method
Hydrocarbon fueled supersonic film cooling is considered to be one of the most promising thermal protection methods for scramjet combustors, while regulating its flow and combustion characteristics and improving its cooling performance are of great significance for engine performance. In this paper, the effects of segmented injection regulation method on hydrocarbon fueled supersonic film cooling performance are numerically investigated. The results indicate that, with single film injection, film combustion first brings beneficial effect and then brings negative effect on the supersonic film cooling. Whereas, segmented injection reorganizes near-wall chemical reaction and flow characteristics, resulting in endothermic-exothermic- endothermic reaction characteristics near the wall, leading to the combustion high-temperature region distributed in the film potential-core flow characteristic region and suppressing the mixing process. Therefore, segmented injection regulation method can significantly shorten the negative effect region brought by the film combustion, and further improve the supersonic film cooling performance based on that with single film injection. It is worth mentioning that, the overall film cooling performance with segmented injection is not sensitive to the flow distribution ratio in the variation range from 5:5 to 7:3. Furthermore, the second film injection arranges at the separation point of the first film, where the combustion begins to have negative effect on the film cooling, can eliminate the negative effect. Within the 500 mm length range without increasing the mass flow rate of film coolant, segmented injection by dual films with flow equalization principle and evenly distributed position can increase the average supersonic film cooling effectiveness by 19 %, and decrease the average wall skin friction by 20.1 %. The forward movement of the second film layout position to the separation point can further increase the average supersonic film cooling effectiveness by 2.85 %.
期刊介绍:
The International Journal of Thermal Sciences is a journal devoted to the publication of fundamental studies on the physics of transfer processes in general, with an emphasis on thermal aspects and also applied research on various processes, energy systems and the environment. Articles are published in English and French, and are subject to peer review.
The fundamental subjects considered within the scope of the journal are:
* Heat and relevant mass transfer at all scales (nano, micro and macro) and in all types of material (heterogeneous, composites, biological,...) and fluid flow
* Forced, natural or mixed convection in reactive or non-reactive media
* Single or multi–phase fluid flow with or without phase change
* Near–and far–field radiative heat transfer
* Combined modes of heat transfer in complex systems (for example, plasmas, biological, geological,...)
* Multiscale modelling
The applied research topics include:
* Heat exchangers, heat pipes, cooling processes
* Transport phenomena taking place in industrial processes (chemical, food and agricultural, metallurgical, space and aeronautical, automobile industries)
* Nano–and micro–technology for energy, space, biosystems and devices
* Heat transport analysis in advanced systems
* Impact of energy–related processes on environment, and emerging energy systems
The study of thermophysical properties of materials and fluids, thermal measurement techniques, inverse methods, and the developments of experimental methods are within the scope of the International Journal of Thermal Sciences which also covers the modelling, and numerical methods applied to thermal transfer.