塑料农膜与农业生产可持续发展

农膜的应用对农业发展做出了不可估量的贡献,但是,长期过量使用化肥、农药和塑料农膜将导致土壤板结,地力下降,水体污染和负营养化,破坏自然生态系统的结构和功能。如何合理使用塑料农膜,确保农业生产可持续发展,是摆在每一位环境保护工作者面前的重要课题。     

Estimating defence budget saving from disarmament: the United States’ case

Probing the technology in the production of US national defence by using a dynamic cost‐function model with adjustment costs, this paper evaluates the effect of reducing the level of national defence on the defence budget saving. Our inquiry involves estimating the defence production structure without output data for non‐market goods that are normally unavailable. Our findings include: (i) the United States behaves rationally to minimize cost in the production of national defence; (ii) the adjustment costs are larger in disarmament than in military build‐up; (iii) due to the adjustment costs peculiar to disarmament, the defence budget saving from disarmament appears small, but cutbacks allow great savings on the defence budget.     

剖分T型钢轴心压杆的弯扭屈曲

《钢结构设计规范》（GB50017—2003）认为单轴对称的T型钢轴心压杆绕对称轴的稳定性是弯扭失稳问题。本次试验发现,剖分T型钢轴压杆有必要做弯扭屈曲验算,计算方法采用换算长系比法。     

空空导弹控制系统一体化设计方法研究

综述了空空导弹控制系统非线性设计的主要理论和方法,重点介绍了非线性动态逆和反馈线性化方法及其在导弹控制系统设计中的应用,对大攻角空空导弹控制系统一体化设计方法进行了分析和展望。     

舰炮武器试验中目标坐标真值修正方法

为保证舰炮武器系统动态精度解算结果的准确性,分析了舰炮武器系统动态精度试验中,GPS作为目标瞬时坐标真值测量设备时,因其安装位置与雷达跟踪测量中心不重合所引起的误差,并提出了一种简便、可行的误差修正方法。给出了误差修正示例,比较分析了GPS不同安装位置所引起的误差,为类似试验中目标瞬时坐标真值的处理提供参考。     

嵌段聚氨酯弹性体的动态力学性能研究

以预聚体法合成了两嵌段聚醚—聚酯型聚氨酯弹性体。研究了配料比、氨酯基浓度及固化剂用量等对该体系动态力学性能的影响。发现:该嵌段共聚物是完全相容的,其玻璃化转变温度T_g与聚醚含量呈线性关系;固化剂用量对该体系的T_g亦有影响。此外,对于聚酯氨酯体系,其T_g值与氨酯基浓度U亦呈线性关系。     

A DYNAMIC PANEL DATA MODEL FOR ANALYZING THE RELATIONSHIP BETWEEN MILITARY EXPENDITURE AND GOVERNMENT DEBT IN THE EU

This paper examines the impact of military spending on general government debt in the enlarged European Union (EU) countries. For this purpose, we use panel data analysis and provide estimates from a dynamic Generalized Method of Moments (GMM) panel model. The dynamics are found to be important and the results suggest that military expenditures do have a large positive impact on the share of general government debt in the EU.     

Multi-objective design optimization of composite submerged cylindrical pressure hull for minimum buoyancy and maximum buckling load capacity

This paper presents the design optimization of composite submersible cylindrical pressure hull subjected to 3 MPa hydrostatic pressure. The design optimization study is conducted for cross-ply layups [0s/90t/0u], [0s/90t/0u]s, [0s/90t]s and [90s/0t]s considering three uni-directional composites, i.e. Carbon/Epoxy, Glass/Epoxy, and Boron/Epoxy. The optimization study is performed by coupling a Multi-Objective Genetic Algorithm (MOGA) and Analytical Analysis. Minimizing the buoyancy factor and maximizing the buckling load factor are considered as the objectives of the optimization study. The objectives of the optimization are achieved under constraints on the Tsai-Wu, Tsai-Hill and Maximum Stress composite failure criteria and on buckling load factor. To verify the optimization approach, optimization of one particular layup configuration is also conducted in ANSYS with the same objectives and constraints.     

How old is too old? An economic approach to replacing military aircraft

The US Air Force is asking when to replace its aging aircraft. We develop a framework to identify economically optimal replacement strategies that recognizes cost trade-offs and incorporates age effects. We also preview a stochastic methodology. We use the framework to identify an optimal strategy, defined by the replacement age, for a generic fleet and conduct a sensitivity analysis. Quantitative illustrations show that the range of strategies that provides close-to-optimal outcomes widens as the operating and support (O&S) cost growth rate decreases and the ratio of the acquisition price to the initial O&S cost increases. A wider range implies more decision-making leeway.     

Formation of adiabatic shearing band for high-strength Ti-5553 alloy: A dramatic thermoplastic microstructural evolution

By using split Hopkinson pressure bar, optical microscopy and electronic microscopy, we investigate the influence of initial microstructures on the adiabatic shear behavior of high-strength Ti–5Al–5V–5Mo–3Cr (Ti-5553) alloy with lamellar microstructure and bimodal microstructure. Lamellar alloy tends to form adiabatic shearing band (ASB) at low compression strain, while bimodal alloy is considerably ASB-resistant. Comparing with the initial microstructure of Ti-5553 alloy, we find that the microstructure of the ASB changes dramatically. Adiabatic shear of lamellar Ti-5553 alloy not only results in the formation of recrystallized β nano-grains within the ASB, but also leads to the chemical redistribution of the alloying elements such as Al, V, Cr and Mo. As a result, the alloying elements distribute evenly in the ASB. In contrast, the dramatic adiabatic shear of bimodal alloy might give rise to the complete lamination of the globular primary α grain and the equiaxial prior β grain, which is accompanied by the dynamic recrystallization of α lamellae and β lamellae. As a result, ASB of bimodal alloy is composed of α/β nano-multilayers. Chemical redistribution does not occur in ASB of bimodal alloy. Bimodal Ti-5553 alloy should be a promising candidate for high performance armors with high mass efficiency due to the processes high dynamic flow stress and excellent ASB-resistance.