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2018 Joint Thermophysics and Heat Transfer Conference最新文献

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LES of an Asymmetrically Heated High Aspect Ratio Duct at High Reynolds Number at Different Wall Temperatures 不同壁温下高雷诺数下非对称加热高展弦比风管的LES
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-4287
Thomas Kaller, S. Hickel, N. Adams
We present the results of well-resolved large-eddy simulations (LES) of an asymmetrically heated high aspect ratio cooling duct (HARCD) with an aspect ratio of AR = 4.3 for two different wall temperatures. The temperature difference with respect to the bulk flow is ∆T = 40 K, respectively ∆T = 60 K. The HARCD is operated with liquid water at a Reynolds number of Reb = 110 ⋅ 103 based on bulk velocity and hydraulic diameter. The generic HARCD setup follows a reference experiment. The main goal of the present study is the numerical investigation of the interaction of turbulent heat transfer and the turbulent duct flow, specifically the heating induced changes in mean flow and turbulent statistics with a spatially developing temperature boundary layer. Furthermore, we investigate the influence of asymmetric wall heating on streamwise vorticity and its dynamics as well as the turbulent Prandtl number and the effect of the secondary flow on its distribution.
本文对长径比为AR = 4.3的非对称加热高长径比冷却管(HARCD)在两种不同壁面温度下的高分辨率大涡模拟(LES)结果进行了研究。相对于整体流量的温差分别为∆T = 40 K,∆T = 60 K。基于体积速度和液压直径,在雷诺数Reb = 110⋅103的液态水条件下操作HARCD。一般的硬碟设置遵循参考实验。本研究的主要目的是对湍流传热和湍流管道流动的相互作用进行数值研究,特别是加热引起的平均流量和湍流统计量的变化与空间发展的温度边界层。此外,我们还研究了不对称壁面加热对流向涡度及其动力学的影响,以及湍流普朗特数和二次流对其分布的影响。
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引用次数: 3
Insights into Catalytic Mechanism of 4MgCO3Mg(OH)25H2O on Thermal Kinetics and Combustion Behavior of 5-amino-1h-tetrazole Based Propellant 4MgCO3Mg(OH)25H2O对5-氨基-1h-四唑基推进剂热动力学和燃烧行为的催化机理研究
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3760
Dan Zhang, Song Lu, Heping Zhang, Changcheng Liu, Cao Chengyang, Lin Jiang, Z. Gao
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引用次数: 1
Diagnostic Investigation of Radiation Effects on Pre-ignition Heat Flux Distribution in Dual Thrust Solid Rockets 辐射对双推力固体火箭点火前热流分布影响的诊断研究
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3765
Vignesh Saravanan, V. Natarajan, S. Anbarasan, R PrasannaT, M Nijanthan, S Vineeshwar, Hemasai N.D, S. Padmanabhan, S. A. Rahman, VR Sanal Kumar
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引用次数: 1
Effects of Zincaluminate on Thermal Behaviors and Combustion Characteristics of 5AT/Sr(NO3)2 Propellant 铝酸锌对5AT/Sr(NO3)2推进剂热性能和燃烧特性的影响
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3911
Cao Chengyang, Song Lu, Dan Zhang, Changcheng Liu, Heping Zhang
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引用次数: 0
Characterization of CO Thermochemistry in Incident Shockwaves CO在入射冲击波中的热化学表征
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3768
B. Cruden, A. Brandis, Megan E. Macdonald
Incident shock waves in pure CO have been characterized in the Electric Arc Shock Tube facility Spectrally and spatially resolved emission spectra characterize radiative signatures from CO in the VUV and mid-infrared and atomic carbon and C 2 in the visible. CO absorption of a single vibrational line is also measured with a tunable diode laser. The experimental data analyzed here are at a pressure of 0.25 Torr in the driven section and span a shock velocity range from 3.4-9.5 km/s. The emission and absorption signals are analyzed to extract temperature relaxation behind the shock which is used to derive the rate of CO dissociation. The emission spectra are compared to results using different kinetic parameters for CO dissociation and C 2 dissociation and exchange. Different rates from the literature are found to match the data from 3.4-6.6 km/s and 6.6-9.5 km/s. Areas for improvement in CO and C 2 radiation modeling are suggested on the basis of the analysis.
在电弧激波管设备上对纯CO中的入射激波进行了表征,光谱和空间分辨发射光谱表征了CO在紫外和中红外波段的辐射特征,以及可见的碳原子和二氧化碳。用可调谐二极管激光器也测量了单个振动线的CO吸收。本文分析的实验数据是在驱动段压力为0.25 Torr,冲击速度范围为3.4-9.5 km/s的情况下进行的。对发射和吸收信号进行分析,提取激波后的温度弛豫,并以此计算CO的解离速率。将发射光谱与不同动力学参数下CO解离和co2解离交换的结果进行了比较。从文献中发现不同的速率与3.4-6.6 km/s和6.6-9.5 km/s的数据相匹配。在此基础上,提出了CO和co2辐射模拟需要改进的地方。
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引用次数: 26
Ignition and Damage Thresholds of Materials at Extreme Incident Radiative Heat Flux 材料在极端入射辐射热流下的点火和损伤阈值
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3764
J. Engerer, Alexander L. Brown, J. Christian
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引用次数: 3
Uncertainty Analysis of Coaxial Thermocouple Calorimeters used in Arc Jets 电弧射流用同轴热电偶量热计的不确定度分析
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3770
D. Driver, D. Philippidis, Imelda Terrazas-Salinas
Recent introduction of Coaxial Thermocouple type calorimeters into the NASA Ames arc jet facilities has inspired an analysis of 2D conduction effects internal to this type of calorimeter. Lateral conduction effects violate the 1D finite slab inverse analysis which is typically used to deduce the heat transfer to such calorimeters. The spherical shaped nose associated with most calorimeters (rather than flat) leads to a bias error that over-estimates the stagnation heating. Non-uniform heating on the face of spherically shaped calorimeters leads to conduction losses to the colder rim of the calorimeter which causes an underestimate of the stagnation heating. These two effects come into play at different times of the calorimeter's exposure to the arc jet, so they do not cancel. The spherical body effects come into play in the early stages of exposure, while the non-uniform heating effect becomes most severe at the later stages of exposure. The bias associated with spherical effects can be avoided by rewriting the 1D finite slab inverse analysis code to solve for 1D conduction in spherical coordinates. However, reducing the bias error associated non-uniform heating requires a somewhat ad hoc modification to the 1D finite element inverse analysis.
最近,同轴热电偶型量热计被引入美国宇航局艾姆斯电弧射流设施,激发了对这种类型量热计内部二维传导效应的分析。横向传导效应违反了一维有限板逆分析,该分析通常用于推断此类量热计的传热。与大多数量热计相关的球形鼻子(而不是扁平的)导致偏差误差,过高估计停滞加热。球形量热计表面的不均匀加热导致量热计较冷边缘的传导损失,从而导致对停滞加热的低估。这两种效应在量热计暴露于电弧射流的不同时间发挥作用,因此它们不会相互抵消。球体效应在曝光初期起作用,而非均匀加热效应在曝光后期最为严重。通过将一维有限板反分析代码改写为在球坐标下求解一维传导,可以避免与球面效应相关的偏差。然而,减少与非均匀加热相关的偏差误差需要对一维有限元逆分析进行一些特别的修改。
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引用次数: 3
Process Optimization of Ceramic Matrix Composites for Ultrasonically Absorptive TPS Material 超声吸收TPS材料陶瓷基复合材料工艺优化
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-2947
C. Dittert, M. Kütemeyer, M. Kuhn, A. Wagner
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引用次数: 2
Aerothermodynamic modelling of meteor entry flows in the rarefied regime 稀薄状态下流星进入流的空气热力学模拟
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-4180
F. Bariselli, S. Boccelli, T. Magin, A. Frezzotti, A. Hubin
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引用次数: 5
Overview of the second test-flight of the Kentucky Re-entry Universal Payload System (KRUPS) 肯塔基再入通用有效载荷系统(KRUPS)第二次试飞概述
Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3589
J. D. Sparks, Alexandre Martin
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引用次数: 8
期刊
2018 Joint Thermophysics and Heat Transfer Conference
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