{"title":"Effect of multi-hole film interactions on thermal protection and drag reduction performances under supersonic condition","authors":"Dingyuan Wei, Jingying Zuo, Jianfei Wei, Xin Li, Silong Zhang, Wen Bao","doi":"10.1016/j.ijthermalsci.2025.110099","DOIUrl":null,"url":null,"abstract":"<div><div>Hydrocarbon-fueled scramjet engines face significant challenges related to aerodynamic frictional drag and thermal protection due to high-speed incoming flow and high-intensity combustion heat release. Multi-hole discrete film injection using gaseous hydrocarbon fuel can effectively reduce frictional drag while enhancing film cooling performance. Numerical simulations based on the Reynolds-Averaged Navier-Stokes method have been conducted to investigate the effect of multi-hole film interactions on thermal protection and drag reduction performances under supersonic condition in a supersonic combustor. The results indicate that multi-hole discrete film jets achieve better cooling efficiency and broader cooling coverage under supersonic incoming flow conditions compared with subsonic incoming flow at the same blowing ratio. Under subsonic condition, the small velocity difference between the multi-hole discrete film jets and the main flow exacerbates the penetration of the transverse jet into the main flow, leading to a decrease in cooling efficiency. Smaller lateral hole spacing (<em>P/D</em>) is better for combustion drag reduction and thermal protection performances under supersonic conditions, as it enables neighboring jets to form anti-kidney-type vortex pair structures and creates a cracking heat absorption region. Furthermore, the axial hole spacing (<em>S/D</em>) in aligned multi-hole discrete film jets significantly enhances thermal protection performance by regulating the chemical reaction of hydrocarbon fuel and extending the cracking reaction region. Secondary hydrocarbon-fueled film injection extends the cracking reaction region and delays the onset of the combustion heat release zone, thereby expanding the effective cooling region. Moreover, an optimization analysis of the cross multi-hole discrete film jet structure shows that cooling coverage increases to 73.5 % at <em>S/D</em> = 10 and <em>P/D</em> = 2, while the hydrocarbon fuel combustion resistance is reduced by 33.2 %.</div></div>","PeriodicalId":341,"journal":{"name":"International Journal of Thermal Sciences","volume":"217 ","pages":"Article 110099"},"PeriodicalIF":4.9000,"publicationDate":"2025-06-26","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/S1290072925004223","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}
引用次数: 0
Abstract
Hydrocarbon-fueled scramjet engines face significant challenges related to aerodynamic frictional drag and thermal protection due to high-speed incoming flow and high-intensity combustion heat release. Multi-hole discrete film injection using gaseous hydrocarbon fuel can effectively reduce frictional drag while enhancing film cooling performance. Numerical simulations based on the Reynolds-Averaged Navier-Stokes method have been conducted to investigate the effect of multi-hole film interactions on thermal protection and drag reduction performances under supersonic condition in a supersonic combustor. The results indicate that multi-hole discrete film jets achieve better cooling efficiency and broader cooling coverage under supersonic incoming flow conditions compared with subsonic incoming flow at the same blowing ratio. Under subsonic condition, the small velocity difference between the multi-hole discrete film jets and the main flow exacerbates the penetration of the transverse jet into the main flow, leading to a decrease in cooling efficiency. Smaller lateral hole spacing (P/D) is better for combustion drag reduction and thermal protection performances under supersonic conditions, as it enables neighboring jets to form anti-kidney-type vortex pair structures and creates a cracking heat absorption region. Furthermore, the axial hole spacing (S/D) in aligned multi-hole discrete film jets significantly enhances thermal protection performance by regulating the chemical reaction of hydrocarbon fuel and extending the cracking reaction region. Secondary hydrocarbon-fueled film injection extends the cracking reaction region and delays the onset of the combustion heat release zone, thereby expanding the effective cooling region. Moreover, an optimization analysis of the cross multi-hole discrete film jet structure shows that cooling coverage increases to 73.5 % at S/D = 10 and P/D = 2, while the hydrocarbon fuel combustion resistance is reduced by 33.2 %.
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.