再入飞行器超高温陶瓷防热应用研究

目的探索尖锥外形高超声速飞行器超高温陶瓷防热设计约束要求。方法基于计算流体力学有限体积数值求解方法研究高超声速层流状态尖锥形飞行器的气动热环境,通过不同攻角下热流及辐射平衡温度分布规律研究获得防热设计约束要求。针对典型尖锥飞行器超高温陶瓷防热设计要求开展几何尺寸、攻角范围影响研究,最后探讨超高温陶瓷高性能热导率对防热设计影响。结果尖锥飞行器高热流仅限于驻点附近很小的区域,迎风面热流随着攻角增大迅速提高。满足防热设计约束的极限飞行攻角与端头长度呈正比,端头长度增加0.1m,极限攻角增大10°。超高温陶瓷热导率对端头防热设计影响较大,随着材料热导率增大50%,驻点辐射平衡温度降低205 K,端头连接结构温度增大50 K。结论尖锥体超高温陶瓷端头防热设计的重要约束指标为端头连接结构温度限制,设计时需要合理优化飞行攻角剖面,选取热导率性能适中的材料。     

再入攻角对弹头锥身气动热环境及结构热响应影响研究

目的分析再入弹头锥身气动热环境及结构热响应,研究再入攻角振荡对其影响规律。方法建立基于工程法的气动热/结构热响应耦合计算方法,并采用该方法开展锥身典型位置气动热环境及结构热性计算分析。结果随着再入攻角的振荡衰减,各典型子午面冷壁热流密度曲线围绕90°子午面热流密度曲线振荡,其振幅呈现先振荡增大、后振荡衰减的变化规律。与90°子午面相比,各子午面总加热量均有所增大。再入攻角振荡引起的金属层外壁面温度最大振荡幅值为3K,但对最终时刻结构温度影响较小。结论计算弹道条件下,再入飞行攻角振荡对气动热环境及结构热响应影响较小,可通过增加余量的方式给予考虑。     

航行体跨音速斜射入水流动特性数值模拟研究

目的 研究航行体跨音速斜射入水的流动特性,获得不同入水攻角下航行体跨音速可压缩入水特性。方法 建立跨音速航行体的几何模型,采用VOF(Volume of Fluid)均相流模型、SST k-ω湍流模型和Zwart空化模型进行数值模拟,并进行液相可压缩修正,对比不同入水攻角下的入水可压缩流动特性,分析绕航行体空泡的发展规律与航行体姿态和受力特性。结果 计算了不同入水攻角下航行体跨音速斜射入水可压缩流动特性,入水攻角对空泡直径几乎没有影响,但不同攻角下,空泡形态随时间的发展明显不同,并且随着正负攻角的增加,空泡的完整性遭到破坏。航行体弹道轨迹偏移量,随正攻角的增大而增加,随负攻角的增大先增加、后减小。航行体水平和垂直受力随正攻角的增大而减小,随负攻角的增大先增大、后减小。结论 在不同入水攻角下,航行体跨音速入水流动结构的发展具有相似性,但是随着攻角的变化,入水空泡结构、弹道偏移、受力特性都发生明显变化。     

壁面马赫数分布规律可控的新型内收缩基准流场设计方法

根据有旋特征线理论,设计出了沿程马赫数下降规律可控的轴对称基准流场,分析了基准流场的几何参数(前缘压缩角及中心体半径)的影响规律,发现选取较小的前缘压缩角和中心体半径有利于得到性能优良的基准流场;然后在设计状态Ma=6时研究了三种典型的马赫数下降规律对这种轴对称流场性能的影响。最后考虑了粘性的影响,并进行了粘性修正探索,结果表明,采用附面层位移厚度修正方法后,基准流场的壁面压力分布和无粘情况吻合良好。      

刚性隔热瓦对舱段结构动特性影响规律分析

目的 分析刚性隔热瓦尺寸、瓦间缝隙大小及热环境对典型舱段结构动特性的影响规律.方法 以刚性隔热瓦式热防护系统的高超声速飞行器舱段结构为研究对象,建立其动力学模型,分别研究自由-自由边界条件下刚性隔热瓦尺寸及瓦间缝隙大小对舱段结构动特性的影响规律.开展热环境下舱段结构的稳态热传导分析,获得热环境下舱段结构的温度场分布,然...     

再入飞行器振动环境工程预示方法

目的 为再入飞行器振动环境设计提供方法 支撑,并为结构设计和地面环境试验条件制定提供载荷输入.方法 分析再入飞行器振动环境主要特征及其诱导因素,结合飞行试验实测振动数据研究小攻角对飞行振动环境的影响规律,辨识出脉动压力与动压、马赫数以及攻角的关系式.在传统脉动压力预测方法 基础上,建立涉及攻角影响的再入飞行均方根脉动压...     

高超声速飞行器翼前缘射流降热研究

目的获得高超声速飞行器翼前缘射流降热机理。方法通过计算流体力学(CFD)方法,针对典型高超声速带翼飞行器开展飞行马赫数为15条件下的射流干扰热环境规律研究,分析无射流翼前缘气动加热特性,确定热流严酷射流开孔区域,分别在翼前缘激波干扰及翼后段布置射流孔,并设计射流流动参数,开展射流总压与来流总压比率在0.002～0.02范围内的流场仿真计算,获得局部流动及表面热流分布特性,针对计算结果进行对比分析。结果随着总压比率逐渐增大,激波干扰以及机翼后段射流孔区域热流均显著降低,降幅达76%～99%。翼中段无射流典型位置总压比率为0.002时热流增高,增幅为11%～24%,随着射流总压增大热流降低,降幅达68%～86%。高射流总压比率局部射流孔前热流增大2倍以上。结论射流影响下降热机理是射流将高温气体推离壁面,局部表面热流显著降低。低射流总压比率亚音速射流作用区域向下游延伸距离短,不会引起局部再附热流增大。高射流总压比率音速射流降热影响向下游明显延伸,增强射流强度可以增加延伸区长度,同时会诱导局部射流孔前再附热流显著增大。     

飞机用7B04铝合金缝隙腐蚀试验及仿真研究

目的开展飞机用7B04铝合金缝隙腐蚀仿真研究,理解缝隙腐蚀机理,找出影响缝隙腐蚀的关键因素。方法分析缝隙腐蚀类型,开展缝隙腐蚀试验,建立缝隙腐蚀数学模型,选择合适的边界条件,利用有限元法进行仿真计算。结果缝隙内pH值分布计算结果与试验测量值一致,缝隙口与外部液体/大气连接时,缝隙内溶液分别呈酸性或碱性。缝隙口溶液电势较低,缝隙口附近的铝合金腐蚀较快,含Al腐蚀产物多集中在缝隙口附近。缝隙宽度在0.1~0.3 mm范围内变化不影响铝合金腐蚀速率;缝隙深度增加,缝隙口与底部溶液电势差增大,铝合金腐蚀面积增大,但铝合金最大腐蚀电流密度不变。电位升高,缝隙内铝合金的腐蚀加剧,电位提高10 m V,腐蚀24 h后缝隙内铝合金界面的腐蚀电流密度增加59倍,Al(OH)_2Cl的最大浓度为自然电位下的30倍。结论缝隙腐蚀主要受缝隙外部阴极还原反应影响,电位对铝合金缝隙腐蚀的影响最大,飞机结构中应避免高电位材料同铝合金直接接触。     

天然气长输管道喷射火事故影响因素模拟分析

利用PHAST软件对天然气长输管道运行压力、泄漏面积、管径、泄漏方向以及风速等因素对喷射火事故的影响进行了定量模拟分析,结果表明:随着运行压力、泄漏面积、管径和风速的增大,伤害半径也随之增大;而随着泄漏方向的扩大,伤害半径则随之减小。     

H62铜合金镀金接触件镀层破损条件下的腐蚀仿真

目的研究镀层破损条件下的盲孔结构腐蚀。方法利用COMSOL软件实现仿真,通过改变镀层破损区距缝隙口距离(W)和缝隙宽度(H)这两个参数,探讨其对腐蚀的影响。结果腐蚀经过极为短暂的初始阶段即进入稳定阶段,且电流在初始阶段远大于稳定阶段,电解质电位、电极电位在初始及稳定阶段完全不同。阳极反应均发生于破损区域,阴极反应在稳定阶段集中于缝隙口。W、H的增大均会使得电流密度有所增大,但当W大于0.7 mm时,其影响十分微弱,可认为处于稳定值。结论镀层破损条件下的腐蚀为阴极氧化还原反应控制的均匀腐蚀,氧气在初始阶段被快速消耗而得不到补充。W在较小时的改变会对腐蚀有所影响,H的增加会加剧腐蚀。     

Perspirable skin: Thermal buckling achieved by complex functionally graded materials

A perspirable skin is a new design concept of thermal protection system that will autonomously reduce the surface temperature in many applications such as reentry and hypersonic vehicles. A unique design features an assembly of tiles, which buckles upon heating. Potentially, a large gap can be generated through this buckling action. These tiles will be assembled and shrink-fitted within an opening on the existing skin. To induce the buckling action, each tile needs to have a unique CTE variation, which causes thermal expansion radially and thermal shrinkage tangentially. This paper concentrates on the fabrication of these tiles made of complex functionally graded materials (FGMs), and presents our effort to design and fabricate these tiles.     

3D numerical investigation of thermally assisted high efficiency ductile machining of nanocrystalline hydroxyapatite

This study investigates the effects of four different variables (initial workpiece temperature, side rake angle, edge radius/feed rate, and nose radius/depth of cut) on ductile regime machining of a bioceramic material known as nanohydroxyapatite (nano-HAP) using 3D numerical simulation. AdvantEdge FEM Version 5.9 is used to conduct turning simulations of the nano-HAP workpiece. Tecplot 360 is used to analyze the results of the simulations. Because the workpiece is thin, the entire workpiece is set to a uniform initial temperature to simulate laser preheating of the material. Initial workpiece temperature, rake angle (side rake angle), edge radius, and nose radius are varied, and the effects of these operating conditions on critical feed are investigated. It is found that critical feed increases as initial workpiece temperature increases, and also as negativity of rake angle increases. For the edge radius, it is concluded that an initial increase causes an increase in critical feed – however, at some value of edge radius, critical feed shows no further increase; for the nose radius, critical feed appears to show no significant dependence.     

Caps and gaps: a computer model for studies on brood incubation strategies in honeybees (<Emphasis Type="Italic">Apis mellifera carnica</Emphasis>)

In addition to heat production on the comb surface, honeybee workers frequently visit open cells (“gaps”) that are scattered throughout the sealed brood area, and enter them to incubate adjacent brood cells. We examined the efficiency of this heating strategy under different environmental conditions and for gap proportions from 0 to 50%. For gap proportions from 4 to 10%, which are common to healthy colonies, we find a significant reduction in the incubation time per brood cell to maintain the correct temperature. The savings make up 18 to 37% of the time, which would be required for this task in completely sealed brood areas without any gaps. For unnatural high proportions of gaps (>20%), which may be the result of inbreeding or indicate a poor condition of the colony, brood nest thermoregulation becomes less efficient, and the incubation time per brood cell has to increase to maintain breeding temperature. Although the presence of gaps is not essential to maintain an optimal brood nest temperature, a small number of gaps make heating more economical by reducing the time and energy that must be spent on this vital task. As the benefit depends on the availability, spatial distribution and usage of gaps by the bees, further studies need to show the extent to which these results apply to real colonies. M. Fehler and M. Kleinhenz contributed equally to this work.     

声子晶体型高速公路声屏障的降噪性能

利用高速公路改扩建工程产生的大量废旧护栏立柱,针对高速公路轮胎-路面主要噪声,建立三种二维气-固型声子晶体声屏障.利用Comsol Multiphysics计算相应的能带结构,并探究带隙的影响因素.结果表明3种形式均可以产生相应的带隙;散射体壁厚大小对于带隙宽度影响很小,但采用空心散射体可以在低频产生一条完全禁带;对散射体进行开口处理可以有效增加低频带隙宽度;当晶格填充率增大至0.5后,随着填充率增大,从高频到低频依次产生完全禁带,且带隙总宽度增大;通过仿真模拟与室内实验相结合的方式验证了声屏障的降噪特性,声屏障在带隙范围内具有良好的降噪性能,相较直立同规格复合板声屏障,低频降噪效果提升1~16dB,高频降噪效果提升1~2dB,但在1600Hz后,声子晶体声屏障降噪效果不及复合板声屏障,降噪效果受周期数影响较大.声子晶体声屏障可实现新型降噪理念与绿色环保的有机结合.     

声子晶体型高速公路声屏障的降噪性能

利用高速公路改扩建工程产生的大量废旧护栏立柱,针对高速公路轮胎-路面主要噪声,建立三种二维气-固型声子晶体声屏障.利用Comsol Multiphysics计算相应的能带结构,并探究带隙的影响因素.结果表明3种形式均可以产生相应的带隙;散射体壁厚大小对于带隙宽度影响很小,但采用空心散射体可以在低频产生一条完全禁带;对散射体进行开口处理可以有效增加低频带隙宽度;当晶格填充率增大至0.5后,随着填充率增大,从高频到低频依次产生完全禁带,且带隙总宽度增大;通过仿真模拟与室内实验相结合的方式验证了声屏障的降噪特性,声屏障在带隙范围内具有良好的降噪性能,相较直立同规格复合板声屏障,低频降噪效果提升1~16dB,高频降噪效果提升1~2dB,但在1600Hz后,声子晶体声屏障降噪效果不及复合板声屏障,降噪效果受周期数影响较大.声子晶体声屏障可实现新型降噪理念与绿色环保的有机结合.     

利用陶瓷工业废料制备再生陶瓷墙地砖

以废弃陶瓷抛光砖粉、陶瓷墙地砖烧成废料为原材料,硼砂作辅助熔剂制备再生陶瓷墙地砖,研究陶瓷抛光砖粉的高温烧结性能及其对再生墙地砖强度的影响,采用SEM测试分析陶瓷抛光砖粉对再生陶瓷制品微观结构的影响。结果表明:抛光砖粉含玻璃相、颗粒细小,有利坯体烧结密实;复掺少量抛光砖粉和硼砂,可提高制品强度。在硼砂掺量为0.5%,陶瓷抛光砖粉为2%、烧成废料为25%的实验条件下,所得再生陶瓷制品强度最高。该方法具有陶瓷工业废料的综合利用率高,制得的再生陶瓷制品强度高等特点。     

Use of coatings to minimise acid emissions during ceramic tile firing

The manufacture of traditional ceramic products (ceramic tiles, roof tiles, and bricks) is often associated with the emission of F, Cl, and S compounds during the firing stage. According to the literature, fluorine emissions can be reduced by adding CaCO₃ to the raw materials mixture used in fabricating these products. However, data available to the authors indicate that this procedure, which has been successfully applied in manufacturing structural ceramics (roof tiles and bricks), is ineffective in ceramic tile manufacture and modifies tile end properties.This paper examines the possibility of reducing such emissions by applying coatings of alkaline-earth carbonates on to the ceramic tile bottom surface to retain the acid compounds emitted during tile firing. The effectiveness of MgCO₃, CaCO₃, SrCO₃, and BaCO₃ coatings for retaining these acid emissions was studied, using the evolved gas analysis (EGA) technique with a TG-DSC-FTIR-QM instrument.The SrCO₃ coating was found to provide the greatest retention, showing that SO₂ and HCl were retained more efficiently than HF. The presence of fluorides, chlorides, and sulphates of Ca, Sr, and Ba was verified in the respective fired coatings, confirming the existence of chemical reactions between the emitted acid compounds and the coating materials at high temperature.