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Characteristic timescales for detonation-based rocket propulsion systems 基于爆炸的火箭推进系统的特征时标
IF 2.2 4区 工程技术 Q3 MECHANICS Pub Date : 2024-05-06 DOI: 10.1007/s00193-024-01174-5
R. T. Dave, J. R. Burr, M. C. Ross, C. F. Lietz, J. W. Bennewitz

Characteristic timescales for rotating detonation rocket engines (RDREs) are described in this study. Traveling detonations within RDREs create a complex reacting flow field involving processes spanning a range of timescales. Specifically, characteristic times associated with combustion kinetics (detonation and deflagration), injection (e.g., flow recovery), flow (e.g., mixture residence time), and acoustic modes are quantified using first-principle analyses to characterize the RDRE-relevant physics. Three fuels are investigated including methane, hydrogen, and rocket-grade kerosene RP-2 for equivalence ratios from 0.25 to 3 and chamber pressures from 0.51 to 10.13 MPa, as well as for a case study with a standard RDRE geometry. Detonation chemical timescales range from 0.05 to 1000 ns for the induction and reaction times; detonation-based chemical equilibrium, however, spans a larger range from approximately 0.5 to (200~upmu )s for the flow condition and fuel. This timescale sensitivity has implications regarding maximizing detonative heat release, especially with pre-detonation deflagration in real systems. Representative synthetic detonation wave profiles are input into a simplified injector model that describes the periodic choking/unchoking process and shows that injection timescales typically range from 5 to (50~upmu )s depending on injector stiffness; for detonations and low-stiffness injectors, target reactant flow rates may not recover prior to the next wave arrival, preventing uniform mixing. This partially explains the detonation velocity deficit observed in RDREs, as with the standard RDRE analyzed in this study. Finally, timescales tied to chamber geometry including residence time are on the order of 100–10,000 (upmu )s and acoustic resonance times are 10–(1000~upmu )s. Overall, this work establishes characteristic time and length scales for the relevant physics, a valuable step in developing tools to optimize future RDRE designs.

本研究描述了旋转引爆火箭发动机(RDRE)的特征时标。旋转爆燃火箭发动机内的行进爆燃产生了一个复杂的反应流场,涉及跨越一系列时间尺度的过程。具体来说,与燃烧动力学(爆轰和爆燃)、喷射(如流动恢复)、流动(如混合物停留时间)和声学模式相关的特征时间都通过第一原理分析进行了量化,以描述 RDRE 的相关物理特性。研究了三种燃料,包括甲烷、氢气和火箭级煤油 RP-2,等效比从 0.25 到 3,腔室压力从 0.51 到 10.13 兆帕,以及标准 RDRE 几何形状的案例研究。诱导和反应时间的引爆化学时间尺度范围为 0.05 到 1000 ns;然而,基于引爆的化学平衡时间尺度范围更大,从大约 0.5 到(200~upmu )s(流动条件和燃料)。这种时间尺度的敏感性对引爆热释放的最大化有影响,特别是在实际系统中的预爆燃。具有代表性的合成爆轰波剖面被输入到一个简化的喷射器模型中,该模型描述了周期性的窒息/起爆过程,并显示喷射时间尺度通常在5到(50~upmu)s之间,这取决于喷射器的刚度;对于爆轰和低刚度喷射器,目标反应物流速可能无法在下一个波到达之前恢复,从而阻碍了均匀混合。这部分解释了在 RDRE 中观察到的起爆速度不足,本研究分析的标准 RDRE 也是如此。最后,与腔室几何形状相关的时间尺度包括停留时间在100-10,000 (upmu )s左右,声共振时间为10-(1000~upmu )s。总之,这项工作为相关物理学建立了特征时间和长度尺度,是开发工具以优化未来 RDRE 设计的重要一步。
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引用次数: 0
Evaluating evidence supporting the relevancy of 4 psi as a blast overpressure value associated with brain health and performance outcomes following low-level blast overpressure exposure 评估支持 4 psi 爆炸超压值与低水平爆炸超压暴露后大脑健康和性能结果相关性的证据
IF 1.7 4区 工程技术 Q3 MECHANICS Pub Date : 2024-04-29 DOI: 10.1007/s00193-024-01170-9
S. S. Sloley, S. M. Turner

Evidence suggests that low-level blast (LLB) overpressure exposure from military heavy weapons training is associated with subclinical adverse brain health and performance (H &P) outcomes. Existing DOD safety policies related to blast overpressure exposure are not specific to LLB-related brain health effects. This study sought to synthesize the available literature and analyze the relevancy of a specific blast metric to LLB exposures and the manifestation of adverse brain H &P outcomes. A literature search yielded 311 unique articles, from which 220 were identified as human studies on LLB published from 2010 to 2021. After more exhaustive exclusion criteria were applied, 14 articles met the criteria for inclusion. Findings on brain H &P changes were examined in relation to quantified LLB measurements (e.g., peak overpressure) to identify trends. Overall, the included studies suggested that alterations of reaction time, a metric for neurocognitive performance, as well as symptom reporting can occur following cumulative LLB exposures above 4 psi (27.6 kPa). Biomarkers and neurosensory changes have not demonstrated consistent associations with LLB exposures. These findings suggest that cumulative blast overpressure exposures above 4 psi (27.6 kPa) based on current measurement methodologies for body-worn sensors may be associated with adverse brain H &P outcomes. Current research efforts seek to better quantify LLB exposure, the relationships between LLB (e.g., intensity, duration, dose) and brain health, as well as to assess brain H &P domains more comprehensively. These efforts will serve to promote a better understanding of the interaction between LLB exposures and adverse brain H &P outcomes.

有证据表明,军事重武器训练中的低水平爆炸(LLB)超压暴露与亚临床不良脑健康和性能(H &P )结果有关。国防部现有的与爆炸超压暴露相关的安全政策并未专门针对与 LLB 相关的脑健康影响。本研究试图综合现有文献,分析特定爆炸指标与低爆暴露的相关性以及脑部 H &P 不良后果的表现。通过文献检索获得了 311 篇文章,其中 220 篇被确定为 2010 年至 2021 年间发表的有关低放炮弹的人类研究。在采用更详尽的排除标准后,有14篇文章符合纳入标准。研究人员结合量化的 LLB 测量值(如过压峰值)对大脑 H &P 变化的研究结果进行了分析,以确定趋势。总体而言,纳入的研究表明,在暴露于超过 4 psi(27.6 kPa)的累积 LLB 后,反应时间(一种神经认知性能指标)以及症状报告都会发生变化。生物标志物和神经感觉的变化并未显示出与 LLB 暴露有一致的联系。这些研究结果表明,根据目前的体戴式传感器测量方法,超过 4 psi (27.6 kPa) 的累积爆炸超压暴露可能与不良的脑 H &P 结果有关。目前的研究工作旨在更好地量化 LLB 暴露、LLB(如强度、持续时间、剂量)与大脑健康之间的关系,以及更全面地评估大脑 H &P 领域。这些努力将有助于更好地理解低辐射暴露与不良脑 Hamp;P 结果之间的相互作用。
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引用次数: 0
Quantitative proteomic profiling in brain subregions of mice exposed to open-field low-intensity blast reveals position-dependent blast effects 暴露于开阔地低强度爆炸的小鼠大脑亚区域的定量蛋白质组特征分析揭示了位置依赖性爆炸效应
IF 1.7 4区 工程技术 Q3 MECHANICS Pub Date : 2024-04-25 DOI: 10.1007/s00193-024-01169-2
M. Jackson, S. Chen, P. Liu, M. Langenderfer, C. Li, H. R. Siedhoff, A. Balderrama, R. Li, C. E. Johnson, C. M. Greenlief, I. Cernak, R. G. DePalma, J. Cui, Z. Gu

The neurological consequences of combat blast-induced neurotrauma (BINT) pose important clinical concerns for military service members and veterans. Previous studies have shown that low-intensity blast (LIB) results in BINT with multifaceted characteristics in mice exposed to open-field blast in prone position. Although the prone position is natural for rodents, experimental models of blast using this position do not represent common scenarios of human standing while being exposed to blast during deployment or military training. In this study, we used our previously developed BINT mouse model of open-field LIB with mice in an upright position and then used quantitative proteomics and multiple bioinformatic approaches to analyze brain tissue taken from multiple subregions during the acute post-injury phase. We identified: (1) region-specific BINT-induced proteome changes, which were significantly and differently influenced by animal positioning (upright vs. prone): the upright positioning caused more significant protein alterations in cortex and cerebellum, which were less significant in striatum as compared to prone position; (2) synapse- and mitochondrion-related damage contributed to BINT in both positions; and (3) some molecular signatures were exclusively and/or oppositely regulated in two positions. This study delineates the molecular signatures of the position-dependent blast effects, indicating the importance of brain–body position for BINT translational studies and for modeling the location and extent of position-related blast injuries.

战斗爆炸诱发的神经创伤(BINT)会对军人和退伍军人的神经系统造成严重的临床影响。先前的研究表明,小鼠在俯卧位暴露于开阔地爆炸环境中时,低强度爆炸(LIB)会导致具有多方面特征的 BINT。虽然俯卧位是啮齿动物的自然姿势,但使用这种姿势的爆炸实验模型并不代表人类在部署或军事训练期间暴露于爆炸时的常见站立情景。在本研究中,我们使用了之前开发的 BINT 小鼠模型,让小鼠以直立姿势进行开阔地 LIB 实验,然后使用定量蛋白质组学和多种生物信息学方法分析受伤后急性期多个亚区域的脑组织。我们确定了(1)特定区域的 BINT 诱导的蛋白质组变化受动物体位(直立与俯卧)的显著不同影响:与俯卧位相比,直立位在皮层和小脑中引起更显著的蛋白质变化,而在纹状体中则不那么显著;(2)在两种体位下,突触和线粒体相关损伤都会导致 BINT;以及(3)在两种体位下,某些分子特征被单独调控和/或相反调控。本研究描述了位置依赖性爆炸效应的分子特征,表明脑-体位置对 BINT 转化研究以及位置相关爆炸损伤的位置和程度建模的重要性。
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引用次数: 0
Blast injury model estimates from multiple overpressure measurement locations on a single person-borne device 从单人携带装置上的多个超压测量位置得出爆炸伤害模型估计值
IF 1.7 4区 工程技术 Q3 MECHANICS Pub Date : 2024-04-24 DOI: 10.1007/s00193-024-01166-5
J.-P. Dionne, J. Levine, A. Makris

Towards a better characterization of the increasing blast overpressure threat, person-borne sensors are being considered for large military population segments potentially subjected to explosive blast and firing of crew served weapons. Training and field data, tracked longitudinally across a soldier’s entire career, can help with the diagnosis of blast injuries and the improvement of standard operating procedures for both explosive forced entry and large weapons firing. However, a current challenge with person-born blast dosimeters resides with the position of the overpressure sensors themselves. Often, the sensors are not fully exposed to the blast locally, resulting in pressure measurements not representative of the blast conditions surrounding an individual. While fielding multiple individual and uncoupled dosimeter units around the body increases the likeliness of catching the representative blast exposure, issues arise from differences in internal clock, potential partial triggering, and the complexity of merging data from different sources. Instead, integrating multiple overpressure sensors pointing in different directions, within a single device that captures and records all data simultaneously, proves highly beneficial for data analysis and interpretation. This paper presents algorithms that combine the overpressure data collected from such multiple coupled sensors for each blast event to minimize the effect of blast directionality. In particular, an algorithm estimating the equivalent side-on blast overpressure is presented, facilitating injury estimates from existing established blast injury models adapted for the outputs from the blast dosimeters. An algorithm is also presented that estimates the orientation or provenance of an explosive blast relative to the soldier.

为了更好地描述日益严重的爆炸超压威胁,正在考虑为可能遭受爆炸冲击波和乘员服役武器射击的大量军事人员配备人载传感器。对士兵整个职业生涯进行纵向跟踪的训练和实战数据有助于诊断爆炸伤害,并改进爆炸强行进入和大型武器发射的标准操作程序。不过,人本爆炸剂量计目前面临的一个挑战是超压传感器本身的位置。通常情况下,传感器并没有完全暴露在爆炸位置,导致压力测量结果不能代表个人周围的爆炸条件。虽然在身体周围部署多个单独的非耦合剂量计单元可以提高捕捉到代表性爆炸暴露的可能性,但内部时钟的差异、潜在的部分触发以及合并不同来源数据的复杂性都会产生问题。相反,将指向不同方向的多个超压传感器集成到一个设备中,同时捕获和记录所有数据,对数据分析和解释大有裨益。本文介绍的算法可将从此类多个耦合传感器收集到的超压数据与每个爆炸事件相结合,以最大限度地减少爆炸方向性的影响。特别是,本文介绍了一种估算等效侧向爆炸超压的算法,有助于根据爆炸剂量计的输出结果,从现有的既定爆炸伤害模型中进行伤害估算。此外,还介绍了一种估算爆炸相对于士兵的方向或来源的算法。
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引用次数: 0
Development of a vapor-based method for seeding alkali metals in shock tube facilities 在冲击管设施中开发基于蒸汽的碱金属播种方法
IF 1.7 4区 工程技术 Q3 MECHANICS Pub Date : 2024-04-15 DOI: 10.1007/s00193-024-01165-6
J. A. Vandervort, S. C. Barnes, C. L. Strand, R. K. Hanson

This note presents a vapor-based seeding apparatus, named the external alkali seeding instrument (EASI), which is designed to introduce alkali metal vapors into experimental facilities without using precursors or large auxiliary equipment. The device vaporizes small amounts of alkali metals, potassium in this work, which are then carried away by an inert gas. In a benchtop flow cell, carrier gas flow rate (6–(200~hbox {cm}^3/hbox {s})) and device temperature (150–(250,^{circ }hbox {C})) most strongly affected potassium-vapor concentrations. Higher values of either quantity lead to increased potassium-vapor concentrations. When using the EASI to seed a shock tube experiment, vapor-phase potassium was detected immediately after the incident and reflected shockwaves using a laser absorption diagnostic. Mole fraction time histories stay within a factor of 2 over the test time as compared with those from a precursor-based seeding approach, which may span multiple orders of magnitude. This suggests potassium is nearly homogeneously distributed throughout the test gas. This design can be extended to other low-vapor-pressure elements, such as other alkalis or sulfur, with minimal modifications. The EASI simplifies seeding for laboratory experiments targeting potassium and other alkali metals—enabling advances in fundamental spectroscopy, diagnostic development, and chemical kinetics.

本说明介绍了一种基于蒸气的播种设备,名为外部碱金属播种仪(EASI),其设计目的是在不使用前驱体或大型辅助设备的情况下,将碱金属蒸气引入实验设施。该装置可蒸发少量碱金属(在本研究中为钾),然后由惰性气体带走。在台式流动池中,载气流速(6-(200~hbox {cm}^3/hbox {s})和设备温度(150-(250,^{circ }hbox {C})对钾蒸汽浓度的影响最大。这两个数值越大,钾蒸汽浓度越高。当使用 EASI 作为冲击管实验的种子时,在入射和反射冲击波之后立即使用激光吸收诊断仪检测气相钾。与基于前驱体的播种方法相比,摩尔分数时间历程在测试时间内保持在 2 倍的范围内,而前驱体播种方法的时间历程可能跨越多个数量级。这表明钾几乎均匀地分布在整个测试气体中。这种设计可以扩展到其他低气压元素,如其他碱或硫,只需做极少的修改。EASI 简化了以钾和其他碱金属为目标的实验室实验的播种过程,从而推动了基础光谱学、诊断开发和化学动力学方面的进步。
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引用次数: 0
Effect of shock impingement location on the fluid–structure interactions over a compliant panel 冲击撞击位置对顺应性面板上流体与结构相互作用的影响
IF 1.7 4区 工程技术 Q3 MECHANICS Pub Date : 2024-04-15 DOI: 10.1007/s00193-024-01162-9
A. Tripathi, J. Gustavsson, K. Shoele, R. Kumar

An experimental investigation was carried out to study the fluid–structure interactions on a compliant panel subjected to an impinging shock wave and an incoming turbulent boundary layer. These experiments were aimed at understanding the time-averaged and unsteady characteristics of fluid–structure interaction at Mach 2. Two shock impingement locations on the panel (aspect ratio of 2.82), namely the central and three-fourths of the panel length, were tested. The shock boundary layer interactions on a rigid flat plate served as a baseline case. Measurements include shadowgraph and surface oil flow visualizations, panel deflections using a capacitance probe, cavity acoustics using a pressure sensor, surface pressures using discrete pressure sensors, and pressure-sensitive paints. Results show that the interaction on the compliant panel is relatively three-dimensional as compared to a rigid plate with a nominally two-dimensional interaction. Pressure fluctuations on the compliant panel are significantly higher than on the rigid plate, and the fluctuation spectra are multi-modal. Strong coupling at some frequencies was observed between the shock and the panel for both shock impingement locations. The present study suggests that for a compliant panel, the shape of pressure spectra is sensitive to the measurement location on the panel, the panel modifies the pressure distribution around the interaction, and the energy in dominant modes depends on the shock impingement location.

为了研究受冲击波和进入的湍流边界层影响的柔性面板上的流固相互作用,进行了一项实验研究。这些实验旨在了解 2 马赫时流体与结构相互作用的时间平均特性和非稳定特性。测试了面板上的两个冲击撞击位置(长宽比为 2.82),即面板长度的中央和四分之三处。刚性平板上的冲击边界层相互作用作为基线案例。测量包括阴影图和表面油流可视化、使用电容探头的面板偏转、使用压力传感器的空腔声学、使用离散压力传感器的表面压力以及压敏涂料。结果表明,与名义上具有二维相互作用的刚性板相比,顺应性面板上的相互作用是相对三维的。顺应性面板上的压力波动明显高于刚性板上的压力波动,而且波动频谱是多模式的。在冲击撞击的两个位置,都观察到冲击与面板之间在某些频率上的强耦合。本研究表明,对于顺应性面板,压力频谱的形状对面板上的测量位置很敏感,面板会改变相互作用周围的压力分布,主要模式的能量取决于冲击撞击位置。
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引用次数: 0
Semi-confined blast loading: experiments and simulations of internal detonations 半密闭爆破加载:内部爆炸的实验和模拟
IF 1.7 4区 工程技术 Q3 MECHANICS Pub Date : 2024-04-08 DOI: 10.1007/s00193-024-01161-w
M. Kristoffersen, F. Casadei, G. Valsamos, M. Larcher, K. O. Hauge, A. Minoretti, T. Børvik

Far-field blast loading has been studied extensively for decades. Close-in, confined, and semi-confined detonations less so, partly because it is difficult to obtain good experimental data. The increase in computational power in recent years has made it possible to conduct studies of this kind numerically, but the results of such simulations ultimately depend on experimental validation and verification. This work thus aims at using reliable experiments to validate and verify numerical models developed to represent blast loading in general. Test rigs consisting of massive steel cylinders with pressure sensors were used to measure the pressure profiles of semi-confined detonations with different charge sizes. The experimental data set was then used to assess numerical models appropriate for simulating blast loading. In general, the numerical results were in excellent agreement with the experimental data, in both qualitative and quantitative terms. These results may in turn be used to analyse structures exposed to internal blast loads, which constitutes the next phase of this research project.

几十年来,人们对远场爆破加载进行了广泛的研究。对近距离、封闭和半封闭爆炸的研究较少,部分原因是难以获得良好的实验数据。近年来计算能力的提高使得以数值方式进行此类研究成为可能,但此类模拟的结果最终取决于实验的验证和确认。因此,这项工作旨在利用可靠的实验来验证和核实为表示一般爆破加载而开发的数值模型。试验台由装有压力传感器的大型钢筒组成,用于测量不同装药量的半密闭爆炸的压力曲线。实验数据集随后用于评估适合模拟爆破加载的数值模型。总体而言,数值结果与实验数据在定性和定量方面都非常吻合。这些结果可反过来用于分析暴露于内部爆炸荷载的结构,这是本研究项目的下一阶段。
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引用次数: 0
Breakdown regime of a shielded vortex interacting with a standing normal shock: a numerical study 与静止法向冲击相互作用的屏蔽漩涡的破裂机制:数值研究
IF 1.7 4区 工程技术 Q3 MECHANICS Pub Date : 2024-04-05 DOI: 10.1007/s00193-024-01163-8
A. Kundu

Numerical simulation results of a convecting shielded vortex interacting with a normal shock using a compact scheme in the convecting upwind and split pressure framework are presented. We explore the parameter space spanned by vortex Mach number and incident Mach number to look for combinations of the parameters which lead to vortex breakdown. The incident and vortex Mach numbers covered are on the higher side, where relatively less information is available. It is well known that for a weak shock, the vortex retains its original shape and for stronger shocks it breaks down. In-between these two extremes, there is a region where the vortex neither retains its original shape nor does it break into small pieces. We determine the vortex breakdown and transition regions that have not so far been reported in shock–vortex interaction studies. A number of cases have been studied, and a vortex breakdown criterion for the cases considered is proposed.

本文介绍了对流屏蔽涡与法向冲击相互作用的数值模拟结果,采用了对流上风和分压框架下的紧凑方案。我们探索了由涡旋马赫数和入射马赫数构成的参数空间,以寻找导致涡旋崩溃的参数组合。所涉及的入射马赫数和涡旋马赫数偏高,可获得的信息相对较少。众所周知,对于较弱的冲击,涡旋会保持原来的形状,而对于较强的冲击,涡旋则会破裂。在这两个极端之间的区域,涡旋既不会保持原来的形状,也不会碎裂成小块。我们确定了迄今为止在冲击-涡旋相互作用研究中尚未报道的涡旋破裂和过渡区域。我们研究了多种情况,并提出了针对所考虑情况的涡破标准。
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引用次数: 0
Bilayer surrogate brain response under various blast loading conditions 双层代脑在各种爆炸加载条件下的反应
IF 1.7 4区 工程技术 Q3 MECHANICS Pub Date : 2024-04-05 DOI: 10.1007/s00193-024-01158-5
C. Norris, B. Arnold, J. Wilkes, C. Squibb, A. J. Nelson, H. Schwenker, J. Mesisca, A. Vossenberg, P. J. VandeVord

Variations in the experimental constraints applied within blast simulations can result in dramatically different measured biomechanical responses. Ultimately, this limits the comparison of data between research groups and leads to further inquisitions about the “correct” biomechanics experienced in blast environments. A novel bilayer surrogate brain was exposed to blast waves generated from advanced blast simulators (ABSs) where detonation source, boundary conditions, and ABS geometry were varied. The surrogate was comprised of Sylgard 527 (1:1) as a gray matter simulant and Sylgard 527 (1:1.2) as a white matter simulant. The intracranial pressure response of this surrogate brain was measured in the frontal region under primary blast loading while suspended in a polyurethane spherical shell with 5 mm thickness and filled with water to represent the cerebrospinal fluid. Outcomes of this work discuss considerations for future experimental designs and aim to address sources of variability confounding interpretation of biomechanical responses.

在爆炸模拟中应用的实验约束条件不同,会导致测量的生物力学反应大相径庭。最终,这会限制研究小组之间的数据比较,并导致对爆炸环境中 "正确 "生物力学的进一步探究。一种新型双层代用脑暴露于由高级爆炸模拟器(ABS)产生的爆炸波中,爆炸源、边界条件和 ABS 的几何形状各不相同。代理脑由作为灰质模拟物的 Sylgard 527(1:1)和作为白质模拟物的 Sylgard 527(1:1.2)组成。在一次爆炸加载下,在额叶区域测量了这种代用脑的颅内压响应,当时代用脑悬浮在一个 5 毫米厚的聚氨酯球形外壳中,外壳中充满了代表脑脊液的水。这项工作的成果讨论了未来实验设计的注意事项,旨在解决干扰生物力学响应解释的变异性来源。
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引用次数: 0
A simple, self-sufficient approach for the design of shock tube driver insert 设计冲击管驱动器插件的简单、自给自足的方法
IF 2.2 4区 工程技术 Q3 MECHANICS Pub Date : 2024-04-05 DOI: 10.1007/s00193-024-01157-6
Y. Tan, Z. Li, R. Mével

Experimental data obtained in shock tubes, including ignition delay-time and species concentration profiles, are among the most significant parameters in combustion studies. Although shock tubes are widely considered as a quasi-ideal reactor for high-temperature studies, it involves a number of non-ideal effects such as a time-dependent pressure increase within the test section. This non-ideal pressure rise induces inaccuracy in the shock tube measurements. To overcome this issue, the driver insert strategy has proven to be successful. Nevertheless, the approaches presented in the literature to design such a driver insert either are not self-sufficient, i.e., they rely on external software, or lack flexibility. In this study, a simple, self-sufficient, fully analytical approach implemented in a MATLAB code has been developed to design a driver insert for the control of the rate of pressure rise in the test volume. The tip and end positions of the insert, as well as the effect of area change ratio on pressure behind reflected shock are obtained by the code. Extensive validation is performed against previous results from the literature and new data generated with several numerical codes.

在冲击管中获得的实验数据,包括点火延迟时间和物种浓度曲线,是燃烧研究中最重要的参数之一。尽管人们普遍认为冲击管是一种用于高温研究的准理想反应器,但它也会产生一些非理想效应,例如试验段内随时间变化的压力上升。这种非理想的压力上升会导致冲击管测量的不准确性。为了克服这一问题,插入驱动器的策略被证明是成功的。然而,文献中介绍的设计这种驱动器插件的方法要么不能自给自足,即依赖外部软件,要么缺乏灵活性。本研究开发了一种简单、自给自足、完全分析的方法,并在 MATLAB 代码中实现,用于设计控制测试体积内压力上升率的驱动插件。该代码得出了插入件的顶端和末端位置,以及面积变化率对反射冲击后压力的影响。根据以前的文献结果和使用若干数值代码生成的新数据进行了广泛的验证。
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引用次数: 0
期刊
Shock Waves
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