Potential Effects of Surface Temperature Variations and Disturbances and Thermal Convection on the Mars InSight HP<Superscript>3</Superscript> Heat-Flow Determination

The HP³ instrument on the InSight lander mission will measure subsurface temperatures and thermal conductivities from which heat flow in the upper few meters of the regolith at the landing site will be calculated. The parameter to be determined is steady-state conductive heat flow, but temperatures may have transient perturbations resulting from surface temperature changes and there could be a component of thermal convection associated with heat transport by vertical flow of atmospheric gases over the depth interval of measurement. The experiment is designed so that it should penetrate to a depth below which surface temperature perturbations are smaller than the required measurement precision by the time the measurements are made. However, if the measurements are delayed after landing, and/or the probe does not penetrate to the desired depth, corrections may be necessary for the transient perturbations. Thermal convection is calculated to be negligible, but these calculations are based on unknown physical properties of the Mars regolith. The effects of thermal convection should be apparent at shallow depths where transient thermal perturbations would be observed to deviate from conductive theory. These calculations were required during proposal review and their probability of predicting a successful measurement a prerequisite for mission approval. However, their uncertainties lies in unmeasured physical parameters of the Mars regolith.     

Water and Volatiles in the Outer Solar System

Space Science Reviews - Space exploration and ground-based observations have provided outstanding evidence of the diversity and the complexity of the outer solar system. This work presents our...     

某重型燃气轮机放气活门及排气管路的改进设计

针对某重型燃气轮机放气系统放气活门在结构设计上存在的问题,经过分析和论证,提出了改进方案,通过计算验证了该方案可以实施。     

欧盟大涵道比涡扇发动机技术研究计划

1引言随着航空发动机技术的飞速发展、市场竞争的日益激烈和环保要求的不断严格,大涵道比涡扇发动机向着费用更低、性能更高和环保更好的方向发展。为此,21世纪,欧盟国家更加重视大涵道比涡扇发动机的技术研究工作,联合实施了高效和环境友好的航空发动机(EEFAE)、大幅度降低飞机噪声对居民区的影响(SILENCE)、电力优化飞机(POA)、环境友好的航空发动机(VITAL)、新型航空发动机方案(NEWAC)等预研计划(如图1所示),开发和验证了更先进常规循环涡扇发动机技术,探索研究了先进循环涡扇发动机技术,以为未来大涵道比涡扇发动机的研制打下…     

Operating characteristics of a high radius pre-swirl cooling system

An experimental investigation into pre-swirl effectiveness and receiver hole discharge coefficient characteristics for a high radius injection pre-swirl cooling systems was carried out on a physically representative experimental rig with a 450 mm diameter rotor.The receiver holes and pre-swirl nozzle were located at a radius of 181 mm and 180 mm respectively.The experimental work was mainly conducted at 5 000～12 000 r/min,4 bar absolute pressure and 1.132 kg/s air supply.The maximum air supply temperature was 190 ℃.Pressure and temperature distributions in the pre-swirl system were examined with an emphasis on the velocity effectiveness of the pre-swirl system as a whole and on the discharge coefficients of the rotating 'receiver holes' in the rotor.The results showed that the velocity effectiveness increased with increasing swirl ratio resulting in reduced blade cooling flow temperature.Different seal flow configurations caused very different effectiveness at different speeds,but outflow through the inner and outer seals always gave the highest effectiveness compared other configurations.Increasing the seal flow rate reduced the effectiveness.For the coefficient of discharge,except for the low speed range,it increased with increase in swirl ratio for most speeds.      

The role of AVDR in linear cascade testing

Linear cascade testing plays an important role in the research and development of turbomachinery and is widely used over the world.The ideal cascade model of a turbomachinery blade row is two-dimensional.In actual linear cascade testing, the flow through the test section converges due to the development of the boundary layer and secondary flow along the sidewall surfaces of the test section.Axial velocity density ratio(AVDR) is adopted to account for the deviation of the tested cascade flow from the ideal 2D model.Among numerous published cascade works, the influence of AVDR on cascade performance is seen to be complicated with many affecting factors, such as those related to cascade/blade geometry and flow conditions.Also, controlling AVDR is limited by the facility capability.Furthermore, real blade-to-blade flow in turbomachines is usually associated with AVDR greater than unity due to limited span of blades between the hub and shroud such that cascade testing without reducing AVDR could be favored sometimes.All these facets add complexity and diversification to the matter.The current paper reviews previous studies and results on AVDR.Consolidated understanding on the role of AVDR and recommendations on how to deal with it in linear cascade testing are provided.      

区间数据回归分析方法

提出区间数据回归分析方法, 建立区间数据回归方程, 给出回归系数的最佳无偏整体估计及其协方差矩阵.详细讨论了工程中常见的极值分布、Weibull分布和正态分布的等尺度和非等尺度(或异方差)线性回归分析.该方法可以将各个不同状态下的区间数据作为一个整体进行统计分析, 具有信息量大、精度高的特点.      

精密装配对空空导弹位标器影响的研究

通过对其自主稳定回路及间隙描述函数频率特性的分析,对间隙装配调试及检测技术提出改进措施,并设计了测隙装置,完善了装配工艺.     

数据融合在纹理识别中的应用

在室内无线通信模型的优化中,需要区分不同的墙壁对象.而对于室内墙壁的图像可以看作是纹理图像.尝试利用数据融合的方法对这些纹理图像进行识别.实验结果表明,数据融合的方法对相似的纹理图像具有较好的识别效果.