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991.
992.
研究了经270℃等温+不同温度回火后的40CrNi2Si2MoVA钢中残余奥氏体(AR)及其在拉伸条件下的连续变化。研究表明:热处理不同,AR形态及分布均有所不同,各自的稳定性也不同。经油淬和等温热处理加300℃回火的40CrNi2Si2MoVA钢中的AR稳定性好,对性能有益;机械不稳定AR的存在使钢性能变坏。在拉伸变形后,板条间的AR转变为未回火板条马氏体,而板条内AR可转变为孪晶马氏体。 相似文献
993.
994.
夏刚%程文科%秦子增 《宇航材料工艺》2003,33(6):1-6
讨论了充气式再入飞行器对柔性热防护系统的具体要求,归纳了柔性热防护系统设计的一般准则。概述了柔性热防护系统在充气式再入飞行器中的应用现状,并指出在多层隔热毡(MLI)外表敷设耐高温涂层是柔性热防护系统的理想方案。介绍了柔性热防护系统的材料技术,指出轻质、柔性和耐高温是柔性热防护材料的主要特征,并建议在充气式再入飞行器的总体设计过程中采用Nextel312作为主要候选材料来完成相应的热防护设计。 相似文献
995.
GRAINSTRUCTURECONTROLOFNICKEL-BASESUPERALLOYSINCASTINGPROCESS:EFFECTOFFOUNDRYVARIABLESGRAINSTRUCTURECONTROLOFNICKEL-BASESUPER... 相似文献
996.
C.T. Russell A.A. Shinde L. Jian 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2005,35(12):2178-2184
The interplanetary manifestations of coronal mass ejections, ICMEs, have many signatures in the solar wind but none of these signatures in the velocity, density, temperature, magnetic field, plasma composition or energetic particles uniquely and unambiguously identifies the occurrence of an ICME. Different investigators identify different events when confronted with the same data. Herein, we present a single physical parameter that combines information from multiple plasma components and that holds the promise of defining a beginning and an end of the region of influence ICME and an indication of the location of the encounter with the ICME relative to its central meridian. This parameter is the total plasma pressure perpendicular to the magnetic field, consisting of the sum of the magnetic pressure and plasma kinetic or thermal pressure. It provides a vehicle for classifying the nature of the ICME encounter and, in many cases, provides an unambiguous start and stop time of the event. However, it does not provide a start and stop time for any embedded flux rope. This identification depends on examination of the magnetic field. 相似文献
997.
E. Romashets M. Vandas 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2005,36(12):2268-2272
It is generally assumed that magnetic fields inside interplanetary magnetic clouds and flux ropes in the solar photosphere are force-free. In order to model such fields, the solution of rot B = B is commonly used where = const. But comparisons of this solutions with observations show significant difference. To treat this problem,we examine the solutions with . 相似文献
998.
Open source feld operation and manipulation(OpenFOAM)is one of the most prevalent open source computational fluid dynamics(CFD)software.It is very convenient for researchers to develop their own codes based on the class library toolbox within OpenFOAM.In recent years,several density-based solvers within OpenFOAM for supersonic/hypersonic compressible flow are coming up.Although the capabilities of these solvers to capture shock wave have already been verifed by some researchers,these solvers still need to be validated comprehensively as commercial CFD software.In boundary layer where diffusion is the dominant transportation manner,the convective discrete schemes'capability to capture aerothermal variables,such as temperature and heat flux,is different from each other due to their own numerical dissipative characteristics and from viewpoint of this capability,these compressible solvers within OpenFOAM can be validated further.In this paper,frstly,the organizational architecture of density-based solvers within OpenFOAM is analyzed.Then,from the viewpoint of the capability to capture aerothermal variables,the numerical results of several typical geometrical felds predicted by these solvers are compared with both the outcome obtained from the commercial software Fastran and the experimental data.During the computing process,the Roe,AUSM+(Advection Upstream Splitting Method),and HLLC(Harten-Lax-van Leer-Contact)convective discrete schemes of which the spatial accuracy is 1st and 2nd order are utilized,respectively.The compared results show that the aerothermal variables are in agreement with results generated by Fastran and the experimental data even if the1st order spatial precision is implemented.Overall,the accuracy of these density-based solvers can meet the requirement of engineering and scientifc problems to capture aerothermal variables in diffusion boundary layer. 相似文献
999.
1000.