Investigation of supercritical cracking characteristics of alkane and cycloalkane for heat sink application in a supersonic engine

IF 5.4 3区 工程技术 Q2 ENERGY & FUELS Thermal Science and Engineering Progress Pub Date : 2025-03-01 Epub Date: 2025-01-26 DOI:10.1016/j.tsep.2025.103306
Madhavaiah Nalabala , Shree Veena Mamilla , Iyman Abrar , Appala Naidu Uttaravalli , Srikanta Dinda
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Abstract

Thermal control around the combustion chamber is a critical issue for a supersonic engine to work efficiently. Active cooling using onboard hydrocarbon fuel can be a potential solution to manage thermal loads. In the present investigation, the pyrolysis characteristics of cyclohexane and n-decane were examined under supercritical environments. Experiments were conducted for a temperature range between 500 °C and 600 °C and at 5.5 MPa pressure, to investigate the extent of cracking, coke deposition, and heat sink behavior of the fuels. The boiling properties, cracking conversion, product composition, carbon-to-hydrogen ratio, gas production, and aniline point of the feed and products were examined using a variety of analytical techniques. Two innovative methods were adopted to estimate fuel conversion and heat sink parameters. The suitability of the newly adopted conversion calculation method was validated from GCMS results. n-Decane showed about 33.4 % cracking conversion, which is 3.6 times higher conversion than cyclohexane at 600 °C and 5.5 MPa. Under the same condition, n-decane exhibited 3.3 times more coke deposition than cyclohexane. The total heat sinks of cyclohexane and n-decane are about 2110 and 2423 kJ/kg, respectively, at 600 °C. The outcome of this investigation can be useful in selecting a suitable hydrocarbon composition to manage the thermal load of an onboard supersonic engine.
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超声速发动机散热器用烷烃和环烷烃超临界开裂特性研究
燃烧室周围的热控制是超音速发动机高效工作的关键问题。使用机载碳氢燃料进行主动冷却可能是控制热负荷的一种潜在解决方案。本文研究了环己烷和正癸烷在超临界环境下的热解特性。实验在500 ~ 600℃的温度范围和5.5 MPa的压力下进行,以研究燃料的裂解程度、焦炭沉积和热沉行为。采用多种分析技术对原料和产品的沸腾特性、裂解转化率、产品组成、碳氢比、产气量和苯胺点进行了检测。采用了两种创新的方法来估计燃料转换和散热器参数。用GCMS结果验证了新采用的转换计算方法的适用性。在600℃、5.5 MPa条件下,正癸烷的裂解转化率为33.4%,是环己烷的3.6倍。在相同条件下,正癸烷的积焦量是环己烷的3.3倍。在600℃时,环己烷和正癸烷的总热沉分别约为2110和2423 kJ/kg。这项研究的结果可以帮助选择合适的碳氢化合物组成来管理机载超音速发动机的热负荷。
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来源期刊
Thermal Science and Engineering Progress
Thermal Science and Engineering Progress Chemical Engineering-Fluid Flow and Transfer Processes
CiteScore
7.20
自引率
10.40%
发文量
327
审稿时长
41 days
期刊介绍: Thermal Science and Engineering Progress (TSEP) publishes original, high-quality research articles that span activities ranging from fundamental scientific research and discussion of the more controversial thermodynamic theories, to developments in thermal engineering that are in many instances examples of the way scientists and engineers are addressing the challenges facing a growing population – smart cities and global warming – maximising thermodynamic efficiencies and minimising all heat losses. It is intended that these will be of current relevance and interest to industry, academia and other practitioners. It is evident that many specialised journals in thermal and, to some extent, in fluid disciplines tend to focus on topics that can be classified as fundamental in nature, or are ‘applied’ and near-market. Thermal Science and Engineering Progress will bridge the gap between these two areas, allowing authors to make an easy choice, should they or a journal editor feel that their papers are ‘out of scope’ when considering other journals. The range of topics covered by Thermal Science and Engineering Progress addresses the rapid rate of development being made in thermal transfer processes as they affect traditional fields, and important growth in the topical research areas of aerospace, thermal biological and medical systems, electronics and nano-technologies, renewable energy systems, food production (including agriculture), and the need to minimise man-made thermal impacts on climate change. Review articles on appropriate topics for TSEP are encouraged, although until TSEP is fully established, these will be limited in number. Before submitting such articles, please contact one of the Editors, or a member of the Editorial Advisory Board with an outline of your proposal and your expertise in the area of your review.
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