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A comprehensive evaluation of different radiation models in a gas turbine combustor under conditions of oxy-fuel combustion with dry recycle

机译:在含氧燃料燃烧和干循环条件下对燃气轮机燃烧室中不同辐射模型的综合评估

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The oxy-fuel combustion is a promising CO2 capture technology from combustion systems. This process is characterized by much higher CO2 concentrations in the combustion system compared to that of the conventional air-fuel combustion. To accurately predict the enhanced thermal radiation in oxy-fuel combustion, it is essential to take into account the non-gray nature of gas radiation. In this study, radiation heat transfer in a 3D model gas turbine combustor under two test cases at 20 atm total pressure was calculated by various non-gray gas radiation models, including the statistical narrow-band (SNB) model, the statistical narrow-band correlated-k (SNBCK) model, the wide-band correlated-k (WBCK) model, the full spectrum correlated-k (FSCK) model, and several weighted sum of gray gases (WSGG) models. Calculations of SNB, SNBCK, and FSCK were conducted using the updated EM2C SNB model parameters. Results of the SNB model are considered as the benchmark solution to evaluate the accuracy of the other models considered. Results of SNBCK and FSCK are in good agreement with the benchmark solution. The WBCK model is less accurate than SNBCK or FSCK. Considering the three formulations of the WBCK model, the multiple gases formulation is the best choice regarding the accuracy and computational cost. The WSGG model with the parameters of Bordbar et al. (2014) [20] is the most accurate of the three investigated WSGG models. Use of the gray WSSG formulation leads to significant deviations from the benchmark data and should not be applied to predict radiation heat transfer in oxy-fuel combustion systems. A best practice to incorporate the state-of-the-art gas radiation models for high accuracy of radiation heat transfer calculations at minimal increase in computational cost in CFD simulation of oxy-fuel combustion systems for pressure path lengths up to about 10 bar m is suggested. (C) 2015 Elsevier Ltd. All rights reserved.
机译:含氧燃料燃烧是来自燃烧系统的有前途的二氧化碳捕集技术。与传统的空气燃料燃烧相比,该过程的特点是燃烧系统中的二氧化碳浓度高得多。为了准确预测含氧燃料燃烧中增强的热辐射,必须考虑到气体辐射的非灰色特性。在这项研究中,通过各种非灰色气体辐射模型,包括统计窄带(SNB)模型,统计窄带模型,在总压力20 atm的两个测试案例下,在3D模型燃气轮机燃烧室中的辐射传热进行了计算。相关k(SNBCK)模型,宽带相关k(WBCK)模型,全光谱相关k(FSCK)模型以及几种灰度气体加权总和(WSGG)模型。使用更新的EM2C SNB模型参数进行SNB,SNBCK和FSCK的计算。 SNB模型的结果被视为评估其他模型准确性的基准解决方案。 SNBCK和FSCK的结果与基准解决方案非常吻合。 WBCK模型的准确性不如SNBCK或FSCK。考虑到WBCK模型的三种公式,就准确性和计算成本而言,多种气体公式是最佳选择。具有Bordbar等人参数的WSGG模型。 (2014)[20]是三个调查的WSGG模型中最准确的。灰色WSSG公式的使用会导致与基准数据的显着偏差,因此不应将其用于预测氧燃料燃烧系统中的辐射热传递。最佳实践是,在压力路径长度高达约10 bar m的氧气燃料燃烧系统的CFD模拟中,以最先进的气体辐射模型实现辐射热传递计算的高精度,同时最大程度地降低计算成本。建议。 (C)2015 Elsevier Ltd.保留所有权利。

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