鼓包诱导斜爆震波的数值研究

为实现低马赫数条件下斜爆震波的快速起爆，以及提高斜爆震波对来流扰动的抗干扰能力，提出了通过在诱导区内设置一个小鼓包来控制斜爆震波起爆的方案，并通过数值求解二维多组分欧拉方程研究了楔面和鼓包诱导的斜爆震波。结果表明：通过在诱导区内设置鼓包可实现斜爆震波的提前起爆；且在较宽马赫数范围内，其起爆位置相对固定。鼓包诱导的斜爆震波主要有强耦合和弱耦合两种起爆形式，起爆形式与鼓包和斜激波的相对位置有关。此外，来流扰动会使楔面诱导的斜爆震波剧烈振荡，不利于斜爆震发动机的稳定工作；鼓包的存在对来流扰动所引发的斜爆震波振荡具有一定的抑制作用。     

Interaction of Rossby waves with the Gulf Stream and Kuroshio using altimetry in a framework of a vortex layer model

In this paper, we show the potential of satellite altimetry to study the interaction of Rossby waves with the shear flow. The Miles-Ribner approach, which was developed in gas dynamics in the 1960 s, is used to describe Rossby waves interacting with the Gulf Stream and Kuroshio areas. The region of interaction is approximated by a nonzonal vortex layer. We apply the main formulations of the problem of a nonzonal vortex layer on the β-plane in the formulation of Miles-Ribner to observations in the real ocean. Earlier, we showed that the interaction of waves with a nonzonal flow gives rise to a new class of solutions, which is absent in the case of a zonal flow. This new class of solutions can be interpreted as the pure emission of Rossby waves by the nonzonal flow. We apply this theoretical approach to the areas of the Gulf Stream and Kuroshio as well. We use for analysis altimetry data available at Copernicus Marine Environment Monitoring Service. The analysis of Hovmöller diagrams in the areas under consideration confirms the previously obtained theoretical conclusions of the problem of the interaction of planetary waves with a nonzonal flow on the β-plane in the formulation of Miles-Ribner. The incident waves, as well as refracted and reflected waves are distinguished. The speed of refracted and reflected waves exceeds the speed of incident waves, which confirms the conclusions about the existence of mechanisms for the amplification of planetary waves when they interact with a nonzonal flow.     

陶瓷基复合材料旋转爆震燃烧室壁面冷却研究

为了降低旋转爆震发动机燃烧室壁面温度，设计了陶瓷基复合材料燃烧室主动冷却结构。对燃烧室主动冷却结构的传热特性进行数值模拟，获得主动冷却燃烧室壁面温度响应和温度分布规律。对燃烧室主动冷却结构进行了模型简化，将模拟旋转爆震波获得的不同壁面温度下的热流密度参数加载在冷却模型上，提高了壁面温度模拟的计算效率。结果表明：燃烧室内壁面热流密度随着壁面温度的升高而降低，扩散区的平均热流密度最大；陶瓷基复合材料燃烧室主动冷却结构可以有效降低燃烧室壁面温度，在相同冷却流量下，矩形冷却截面的冷却效果优于圆形冷却截面，可以将燃烧室壁面的温度降到1 200 K以下；燃烧室壁面最高温度在燃烧室中段区域。     

Response of quasi-10-day waves in the MLT region to the sudden stratospheric warming in March 2020

We present an analysis of the response of quasi-10-day waves (Q10DWs) to the sudden stratospheric warming (SSW) event which occurred on March 23, 2020. The Q10DWs are observed in the mesosphere and lower thermosphere (MLT) region by three meteor radars, which are located at middle latitudes along the 120°E meridian from Mohe (MH, 53.5°N, 122.3°E), Beijing (BJ, 40.3°N, 116.2°E), to Wuhan (WH, 30.5°N, 114.6°E). The Q10DWs reveal similar temporal and altitudinal variations during the SSW in the MLT region at the three stations. The activities of Q10DWs are also captured in the temperature measurements from the Sounding of the Atmosphere using Broadband Emission Radiometry (SABER) on the Thermosphere Ionosphere Mesosphere Energetics and Dynamics satellite in the MLT region. Further analysis of the Q10DW phases indicates that the Q10DWs might be in situ generated due to mesospheric instabilities at higher latitudes around MH and then propagate southward to lower latitudes at BJ and WH. The atmospheric instabilities are not directly responsible for the excitations of Q10DWs at lower latitudes, while the observed equatorward propagation of the Q10DWs is important. Our result provides the observational evidence for latitudinal couplings in the MLT region after the SSW onset, which is achieved by southward propagating planetary waves in the MLT region.     

脉冲爆震发动机中温度和组分浓度测量技术的发展

脉冲爆震发动机内部工作条件极其恶劣,测量爆震波温度和某组分浓度十分困难。本文回顾了近几年国内外在爆震温度场测量方面的技术发展,特别是应用激光诊断技术测量爆震波的温度和某些组分浓度。总结了国内外应用光学诊断技术测得的爆震波火焰温度,结果发现:对气体燃料/氧气而言,在化学恰当比下一般其爆震波温度大约为3900K,与CJ理论值非常接近;然而对液态燃料JP-10而言,当氧化剂为氧气时,爆震波温度为2500K;当氧化剂为空气时,爆震波温度仅仅约为1500K。     

Oblique detonation wave triggered by a double wedge in hypersonic flow

Pressure-gain combustion has gained attention for airbreathing ramjet engine applications owing to its better thermodynamic efficiency and fuel consumption rate. In contrast with traditional detonation induced by a single wedge, the present study considers oblique shock interactions attached to double wedges in a hypersonic combustible flow. The temperature/pressure increases sharply across the interaction zone that initiates an exothermic reaction, finally resulting in an Oblique Detonation Wav...