过渡金属氧化物催化作用的表征

本文系统地研究了TMO(过渡金属氧化物)对AP热分解性能和AP/AI/HTPB推进剂燃速的催化作用.结果发现,TMO对AP热分解反应和AP/AI/HTPB推进剂燃速的催化作用是一致的.文中指出了与AP热分解反应和AP/AI/HTPB推进剂燃速同时有关的表征参数,为采用热分析实验预估含铝推进剂的燃速奠定了基础.     

利用转移矩阵进行姿态控制

传统欧拉角控制方法在处理大姿态角机动时往往出现奇异和交联问题。针对这一问题对欧拉角的跳变现象进行了讨论,并从飞行器实际姿态与需求姿态之间的空间关系入手,给出了一种消除欧拉角跳变现象的有效方法－转移矩阵法,仿真计算表明,该方法在大型航天器的姿态控制中可以有效地消除欧拉角奇异、交联和跳跃现象,在欧拉角跳变的情况下仍然能够实现对飞行器的控制。     

A multi-strategy pigeon-inspired optimization approach to active disturbance rejection control parameters tuning for vertical take-off and landing fixed-wing UAV

In this paper, Active Disturbance Rejection Control(ADRC) is utilized in the pitch control of a vertical take-off and landing fixed-wing Unmanned Aerial Vehicle(UAV) to address the problem of height fluctuation during the transition from hover to level flight. Considering the difficulty of parameter tuning of ADRC as well as the requirement of accuracy and rapidity of the controller, a Multi-Strategy Pigeon-Inspired Optimization(MSPIO) algorithm is employed. Particle Swarm Optimization(PSO), Gen...     

环形浅液池内低Prandtl数流体超临界热毛细对流演化

为研究低Prandtl数（Pr）流体热毛细对流演化过程,对环形浅液池内Pr=0.011的流体热毛细对流进行三维数值模拟.研究发现：当Marangoni数较小时,流动为轴对称稳态流动;当Marangoni数超过某一临界值后,流动失稳并转变为热流体波,其波数随Marangoni数增加而减小,而波动主频增大;随着Marangoni数增加,流动加强,沿周向运动的热流体波演变为沿径向运动的径向波,其波数大大减小;当Marangoni数继续增加时,波动频谱曲线噪声增加,呈广谱特性.因此,在计算范围内热毛细对流的演化过程为：轴对称稳态流动-热流体波-单周期径向波-多周期三维振荡流动.     

Robust design of NLF airfoils

 A robust optimization design approach of natural laminar airfoils is developed in this paper. First, the non-uniform rational B-splines (NURBS) free form deformation method based on NURBS basis function is introduced to the airfoil parameterization. Second, aerodynamic characteristics are evaluated by solving Navier-Stokes equations, and the γ-Re_θt transition model coupling with shear-stress transport (SST) turbulent model is introduced to simulate boundary layer transition. A numerical simulation of transition flow around NLF0416 airfoil is conducted to test the code. The comparison between numerical simulation results and wind tunnel test data approves the validity and applicability of the present transition model. Third, the optimization system is set up, which uses the separated particle swarm optimization (SPSO) as search algorithm and combines the Kriging models as surrogate model during optimization. The system is applied to carry out robust design about the uncertainty of lift coefficient and Mach number for NASA NLF-0115 airfoil. The data of optimized airfoil aerodynamic characteristics indicates that the optimized airfoil can maintain laminar flow stably in an uncertain range and has a wider range of low drag.     

γ-Re_θ转捩模型在高超声速下的应用及分析

为了初步研究γ-Reθ转捩模型在高超声速领域的适用性,在自行开发的CFD程序中添加了该模型,利用T3系列平板算例对该模型的实现进行了验证;针对高超声速流动,选取压缩面绕流和双圆锥扰流等算例,分别利用该转捩模型、全层流模拟、以及传统的湍流模型进行了数值模拟计算,并与实验结果进行对比。计算结果表明,尽管该转捩模型是在低速流动的基础上发展的,它仍能准确预测高超声速流动下的转捩现象。     

On early cognitive mapping

In this paper we examine the nature of theearly cognitive map – the beginnings of acognitive map formed from one's earlyimpressions of the environment one is in. Twodistinct paradigms have emerged from ourstudies of what information is initially identified in a cognitive map. The first, which weterm a space-based approach, emphasises makingexplicit the spatial extent of the currentlocal environment. The second emphasises makingexplicit the relationships between objects inthe local environment and we call this anobject-based approach. For both paradigms weexamine the psychological literature to findsupport for the approach and the roboticists'attempts at implementing the idea. We arguethat a space-based approach is the moreappropriate way to compute an early cognitivemap. In particular, we find that Siegel andWhite's (1975) object-based hypothesis, whichstates that the developmental progression of acognitive map is from landmark to route tosurvey map, is not supported. The space-basedparadigm underpins our own work in this areaand we outline our own space-based theory forcomputing an early cognitive map.     

对 k-ω 湍流模型的改进

为了更适合于较复杂几何外形的数值计算，本文提出仅引入１个参数来改进ｋ－ω湍流模型并采用了一种双网格系统的有限体积格式来求解Ｎ－Ｓ方程与改进的的ｋ－ω模型方程。通过平板附面层的计算结果表明了用本文提出的对ｋ－ω湍流模型的改进对控制转捩是有效的。     

Coupling of the coronal he abundance to the solar wind

Models of the transition region — corona — solar wind system are investigated in order to find the coronal helium abundance and to study the role played by coronal helium in controlling the the solar wind proton flux. The thermal force on -particles in the transition region sets the flow of helium into the corona. The frictional coupling between -particles and protons and/or the electric polarization field determines the proton flux in the solar wind as well as the fate of the coronal helium content.     

Menter转捩模型在高超声速流动模拟中的改进及验证

通过压力梯度参数和湍流普朗特数的修正,对Menter等构造的低速经验关系式转捩模型进行了改进,将基于局部信息的Menter转捩模型用于高超声速流动转捩数值模拟。在多个高超声速尖锥转捩流动模拟中,对改进后模型的可靠性进行了检验,算例考核了不同壁面温度、来流湍流度、流向压力梯度等多种流动条件。结果表明,数值计算和风洞试验的壁面温度、温度恢复因子和热流等符合得较好,修正后模型较好地模拟了转捩起始位置和转捩区长度,在高超声速边界层转捩预测中具有一定潜力。