双锥侧向喷流的数值模拟研究

利用侧向喷流进行导弹姿态、轨迹控制是近年来导弹空气动力学前沿热点问题之一。要成功地设计以侧向喷流控制为基础的导弹,必须分析喷流与来流干扰对气动性能的影响。本文采用AUSM 上风格式空间离散三维可压缩非定常NS方程组,数值模拟了双锥侧向喷流干扰流动。将表面压力分布与文献中试验值、计算值进行比较,给出了干扰流场结构,分析了喷流干扰对双锥气动力、力矩的影响。     

旋翼干扰下的直升机尾桨气动噪声计算研究

针对旋翼干扰下的直升机尾桨气动噪声计算问题,将CFD方法与Farassat 1A(F1A)公式相结合,提出了一种适用于旋翼干扰下的尾桨气动噪声数值计算方法。首先,应用所提出的方法进行了噪声的算例验证,并与参考文献结果进行了对比;然后,着重针对悬停和前飞状态旋翼干扰下的尾桨噪声及气动特性进行了计算分析,并与孤立尾桨状态进行了对比。计算分析结果表明:悬停状态下,旋翼干扰下的尾桨气动噪声水平显著大于孤立尾桨;而在前飞状态,由于旋翼尾迹对尾桨桨盘平面产生更强的气动干扰,这一现象会更加明显;同时,在旋翼干扰作用下,尾桨噪声的主传播方向也会发生明显变化。     

利用多卫星观测CIR事件演变的统计分析

根据2007-2009年STEREO-BEHIND (STB)和ACE卫星的行星际磁场和太阳风数据, 基于冕洞高速流从太阳向外匀速径向传输假设, 讨论了随着STB和ACE卫星与太阳之间的夹角从0°增大至70°时, 冕洞发出的高速太阳风形成的相互作用区(CIR)依次扫过STB和ACE卫星的时间差特性, 并统计分析了两颗卫星观测到的CIR参数的变化特征. 结果显示, 可以利用STB对CIR事件的观测来预测这个CIR事件到达ACE的理论时间, 时间误差均值和最大值分别为0.217d和0.952d, 时间误差的产生与STB和ACE卫星观测到的CIR速度大小的不同有关, 用速度差异矫正后, 时间误差的平均值和最大值可分别减小为0.194d 和0.489d; STB和ACE卫星观测的CIR事件太阳风速度最大值的线性相关系数达到了0.84, STB和ACE卫星观测到的CIR事件对特征物理量中速度、质子温度的变化最小, 而质子密度及总压力的变化最大. 分析结果表明, STB和ACE卫星观测到的CIR事件有很强的相似性, STB卫星的CIR观测可以作为ACE卫星观测CIR事件特征的参考, 从而为地球空间环境扰动预报提供依据.      

热斑对涡轮级转静干涉噪声影响数值研究

利用结合相位延迟方法的求解器,对进口有热斑存在的某高压涡轮级流场进行三维非定常计算,然后利用模态匹配方法在涡轮转子下游管道中提取出转静干涉离散噪声信息.通过与进口无热斑存在算例比较表明:在一倍叶片通过频率下,向下游传播的转静干涉离散噪声总声功率级增加了约5.9dB;在二倍叶片通过频率下增加了约11.6dB.      

凹腔前缘角对超声速燃烧室性能的影响

针对带有不同前缘角的凹腔内流动和燃烧过程,分别在冷态和燃烧条件下探讨了前缘角对凹腔内流动损失及阻力特性的影响.研究表明:在壁面垂直喷射的喷口上游和凹腔内部均会形成低速、高温回流区,有利于点火及火焰稳定,燃烧反压通过边界层的亚声速区域上传,形成激波/边界层干扰结构.减小前缘角,可使剪切层分离位置提前,更偏向凹腔内部,导致凹腔后壁面再附激波增强,进而增大了总压损失,降低了总压恢复系数;亦可导致凹腔前、后壁面压差阻力增大,阻力系数上升.进一步认识了凹腔内部流场及稳焰增混机理,进而为优化凹腔结构设计提供依据.      

Analysis of blade vibration response induced by rotating stall in axial compressor

An experimental and numerical study was conducted to investigate the forced response of blade vibration induced by rotating stall in a low speed axial compressor. Measurements have been made of the transient stalling process in a low speed axial compressor stage. The CFD study was performed using solution of 3-dimensional Navier-Stokes equations, coupled with structure finite element models for the blades to identify modal shapes and structural deformations simultaneously. Interactions between fluid and structure were managed in a coupled manner, based on the interface information exchange until convergence in each time step. Based on the rotating stall measurement data obtained from a low speed axial compressor, the blade aeroelastic response induced by the rotating stall flow field was analyzed to study the vibration characteristics and the correlation between the phenomena. With this approach,good agreement between the numerical results and the experimental data was observed. The flow phenomena were well captured, and the results indicate that the rotating field stall plays a significant role in the blade vibration and stress affected by the flow excitation.      

Acceleration of energetic particles by whistler waves in active space experiment with charged particle beams injection

In this paper the investigation of wave-particle interaction during simultaneous injection of electron and xenon ion beams from the satellite Intercosmos-25 (IK-25) carried out using the data of the double satellite system with subsatellite Magion-3 (APEX). Results of active space experiment devoted to the beam-plasma instability are partially presented in the paper Baranets et al. (2007). A specific feature of the experiment carried out in orbits 201, 202 was that charged particle flows were injected in the same direction along the magnetic field lines B₀ so the oblique beam-into-beam injection have been produced. Results of the beam-plasma interaction for this configuration were registered by scientific instruments mounted on the station IK-25 and Magion-3 subsatellite. Main attention is paid to study the electromagnetic and longitudinal waves excitation in different frequency ranges and the energetic electron fluxes disturbed due to wave-particle interaction with whistler waves. The whistler wave excitation on the 1st electron cyclotron harmonic via normal Doppler effect during electron beam injection in ionospheric plasma are considered.     

Planetary wave coupling of the atmosphere–ionosphere system during the Northern winter of 2008/2009

This paper presents the global spatial (latitude and altitude) structure and temporal variability of the ∼23-day ionospheric zonally symmetric (s = 0) planetary wave (PW) seen in the Northern winter of 2008/2009 (October 2008–March 2009). It is shown that these ∼23-day ionospheric oscillations are forced from PWs propagating from below. The COSMIC ionospheric parameters f_oF2 and h_mF2 and electron density at fixed altitudes and the SABER temperatures were utilized in order to define the waves which are present simultaneously in the atmosphere and ionosphere. The long-period PWs from the two data sets have been extracted through the same data analysis method. The similarity between the lower thermospheric ∼23-day (s = 0) temperature PW and its ionospheric electron density response provides valuable and strong experimental evidence for confirming the paradigm of atmosphere–ionosphere coupling.     

旋翼桨-涡干扰气动特性计算及参数影响研究

建立了一个适用于旋翼桨-涡干扰(BVI)气动特性分析的数值方法。在该方法中,控制方程采用惯性坐标系下的非定常Euler方程,以适合于分析BVI流场的特点;为便于前飞流场分区求解和信息传递,使用了嵌套网格方法;对于流场中涡线的模拟,建立了一种适用于有限体积格式的涡引入方法——广义网格速度法,以简化计算。应用上述方法对旋翼BVI流场进行了计算,并与可得到的试验数据进行对比,验证了方法的有效性。通过对比桨叶弦向位置压强的变化得出,在旋翼BVI过程中,气动载荷主要来自桨叶10%弦长内的前缘部分的压强突变。文中还进一步分析了涡强、干扰距离和干扰角度对BVI气动特性的影响。本文的BVI数值计算表明:当涡接近桨叶前缘时,升力达到最大;而涡位于后缘位置时,诱导速度改变桨叶环量分布,破坏了后缘的库塔条件,但随着涡的远离,桨叶表面环量开始重构。     

笔式草图的增量识别

针对笔式三维建模技术中手势交互的特点,提出了一种二维草图的增量识别方法:从原始笔划的在线识别与线元转换,到约束关系的自动捕捉与施加,到二维组合图元的识别与规整,到特征手势的识别,到最后的三维特征建模.整个识别过程依据了三维特征建模思想和基于上下文感知的智能推理技术,通过分层识别的方法从紊乱、非精确的二维草图中有效提取三维建模的特征信息,有效降低了草图识别过程的复杂度和积累误差.将特征手势遵循隐式映射机制映射到三维空间后,实时完成三维建模,实现了二维手绘草图与三维精确建模的有效集成.该方法已经在自主开发的原型系统PenSketch3D中得以验证,并取得良好效果.