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Numerical simulation of the infrared radiative signatures of liquid and solid rocket plumes

机译:液体和固体火箭羽流红外辐射特征的数值模拟

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In this paper, a finite volume method was developed to compute the infrared radiative signatures of both liquid and solid rocket plumes, and to investigate the radiative signatures on two wavebands, 2-6 and 8-12 μm bands, respectively. This method is based on the radiative transport equation for local thermodynamic equilibrium, which accounts for radiative heat transfer in inhomogeneous emitting, absorbing, and non-isotropic scattering media. The radiative properties of combustion gases are computed by using the Elsasser narrow band model, and that of particles are computed by using the Mie scattering theory. A numerical method is applied to solve the following three problems. The first one is the computation of the radiative heat transfer in an absorbing, emitting and isotropic scattering homogeneous cylindrical medium in which the radiative flux is presented. The other two are the computations of the infrared radiation of plumes from the liquid and solid rockets in which both the source and apparent radiant intensities are presented as results. The atmospheric absorption effect on the radiation of plumes is also considered by calculating the atmospheric transmittance using MODTRAN. Some of these results, compared with those available in the literature, have shown satisfactory agreement in most cases.
机译:本文提出了一种有限体积方法来计算液体和固体火箭羽的红外辐射特征,并研究分别在2-6和8-12μm波段的两个波段的辐射特征。此方法基于用于局部热力学平衡的辐射输运方程,该方程解释了在不均匀的发射,吸收和非各向同性散射介质中的辐射热传递。使用Elsasser窄带模型计算燃烧气体的辐射特性,并使用Mie散射理论计算颗粒的辐射特性。应用数值方法来解决以下三个问题。第一个是在吸收,发射和各向同性散射的均匀圆柱介质中辐射热传递的计算,其中呈现了辐射通量。另外两个是来自液体和固体火箭的羽流的红外辐射的计算,其中源和视辐射强度均作为结果给出。还可以通过使用MODTRAN计算大气透射率来考虑大气对烟羽辐射的吸收效应。与文献中的结果相比,这些结果中的一些在大多数情况下已显示出令人满意的一致性。

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