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大型壳体结构内壁轴向非分段式热环境试验研究 被引量:2
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作者 吴大方 潘兵 +2 位作者 王岳武 周岸峰 朱林 《导弹与航天运载技术》 北大核心 2014年第2期44-47,共4页
建立大型壳体结构轴向非分段式高温热试验装置。设计直径为14 mm、长度为2.25 m,长度/直径比接近160的超长大功率石英灯加热器,并使用自行研制的大功率可调式供电装置,提高单区域大面积加热源的调控能力,实现2.1 m的大型壳体结构单区域... 建立大型壳体结构轴向非分段式高温热试验装置。设计直径为14 mm、长度为2.25 m,长度/直径比接近160的超长大功率石英灯加热器,并使用自行研制的大功率可调式供电装置,提高单区域大面积加热源的调控能力,实现2.1 m的大型壳体结构单区域整体连续加热试验研究。该方法有效提高了大型壳体结构内壁试验温度分布的均匀性和真实性,为研制大型高速航天飞行器提供更加良好的高温热环境试验手段。 展开更多
关键词 气动热模拟 壳体结构 石英灯加 试验
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高超声速飞行器前缘流固耦合计算方法研究 被引量:16
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作者 聂涛 刘伟强 《物理学报》 SCIE EI CAS CSCD 北大核心 2012年第18期281-287,共7页
对高超声速流场和结构温度场进行了耦合计算分析,同时基于准静态假设对结构应力进行了分析.流场部分采用基于非定常Navier-Stokes(N-S)方程的有限体积法,湍流模型采用SSTk-ω模型,固体部分采用基于非稳态热传导方程的有限元法,同时基于... 对高超声速流场和结构温度场进行了耦合计算分析,同时基于准静态假设对结构应力进行了分析.流场部分采用基于非定常Navier-Stokes(N-S)方程的有限体积法,湍流模型采用SSTk-ω模型,固体部分采用基于非稳态热传导方程的有限元法,同时基于准静态假设对固体结构的应力应变进行了分析.在流固交界面处,高速流体从固体结构得到温度边界条件,固体结构从高速流体得到热流边界条件,从而实现了流场和固体温度场的紧耦合计算.通过与超声速无限长圆管绕流试验结果进行对比,验证了该方法的可靠性.同时对二维圆管结构在气动加热过程中的温度、应力等的变化进行了比较详细的分析.研究结果表明:随着气动加热时间的推进,由于圆管结构的高温区在不断扩大,导致了结构的热变形在不断地增大;圆管最小变形区出现在θ为60°处;同时研究发现在计算时间内圆管热变形对外部流场的影响可以忽略不计. 展开更多
关键词 高超声速 数值模拟 气动 耦合
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Computations of Inlet/Isolator for SCRAMjet Engine
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作者 Wang Xiaodong,Le Jialing (China Aerodynamics Research & Development Center, R.O. Box 211, Mianyang Sichuan, 621000, China ) 《Journal of Thermal Science》 SCIE EI CAS CSCD 2000年第4期334-338,共5页
The inlet/isolator is one of the important parts to the SCRAMjet engine. In the present paper, the flow fields within an inlet and isolator of a SCRAMjet engine have been simulated by the Reynolds-Averaged Navier-Stok... The inlet/isolator is one of the important parts to the SCRAMjet engine. In the present paper, the flow fields within an inlet and isolator of a SCRAMjet engine have been simulated by the Reynolds-Averaged Navier-Stokes equations with the Baldwin-Lomax algebraic turbulence model. The second order H. C. Yee TVD scheme is used for the inviscid flux terms and a central difference considering the character of flow is used for the diffusion terms. The code was used to simulate the flow field of three types of the inlet/isolator models. The results show that the configuration of the internal compression surface of the inlet and the divergent angle of the isolator have a great important effect on the characteristics of the inlet/isolator. 展开更多
关键词 INLET numerical simulation Navier-Stokes equations turbulence model.
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Lattice Boltzmann Simulation for Complex Flow in a Solar Wall
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作者 陈柔 邵九姑 +2 位作者 郑友取 俞慧丹 许友生 《Communications in Theoretical Physics》 SCIE CAS CSCD 2013年第3期370-374,共5页
In this letter,we present a lattice Boltzmann simulation for complex flow in a solar wall system which includes porous media flow and heat transfer,specifically for solar energy utilization through an unglazed transpi... In this letter,we present a lattice Boltzmann simulation for complex flow in a solar wall system which includes porous media flow and heat transfer,specifically for solar energy utilization through an unglazed transpired solar air collector(UTC).Besides the lattice Boltzmann equation(LBE) for time evolution of particle distribution function for fluid field,we introduce an analogy,LBE for time evolution of distribution function for temperature.Both temperature fields of fluid(air) and solid(porous media) are modeled.We study the effects of fan velocity,solar radiation intensity,porosity,etc.on the thermal performance of the UTC.In general,our simulation results are in good agreement with what in literature.With the current system setting,both fan velocity and solar radiation intensity have significant effect on the thermal performance of the UTC.However,it is shown that the porosity has negligible effect on the heat collector indicating the current system setting might not be realistic.Further examinations of thermal performance in different UTC systems are ongoing.The results are expected to present in near future. 展开更多
关键词 solar wall system complex flow lattice Boltmann similation
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