吸气式高超声速推进助推段内流振荡及其抑制

为了掌握高超声速飞行器盲腔流场的激波振荡机理,采用"双时间步"方法对轴对称吸气式高超声速飞行器内流道盲腔流场进行了非定常数值模拟。结果表明,飞行器内流道出现了非定常激波振荡现象,内流道壁面压力出现了低频高幅的周期性变化。为了消除高超声速飞行器内流道的激波振荡现象,设计了级间段泄流方案,对飞行器进行了内外流一体化定常和非定常的数值模拟。结果表明,级间段泄流方案可以有效地消除内流道的激波振荡现象。     

网络营销和传统营销的差异分析与整合

网络营销是随着计算机和网络技术的发展,在传统营销的基础之上发展起来的一种营销模式,是企业营销战略中的一部分。通过网络营销和传统营销的差异的分析,阐述了网络营销对传统营销的冲击,并提出只有网络营销和传统营销进行整合,优势互补,才能更好的促销营销市场的发展和完善。     

基于变步长LMS算法的空域抗干扰技术研究

信息传输的可靠性、安全性和实时性在国防应用中至关重要。针对复杂且电磁干扰强的战场环境下所需有用信息无法准确接收以及多模块集成化等问题,本文创建函数,经蒙特卡洛实验计算出参数最优值,提出了一种基于椭圆函数的变步长LMS自适应波束形成算法。对比本文算法与其他算法达到稳态的时间,结果表明：在保证稳态误差的前提下,该算法在收敛速度上优于已有的变步长LMS算法,并且运算量小。通过模拟不同来波方向的干扰信号绘制波束方向图,仿真结果证明本文算法指向性强,对干扰的抑制度高,可以实现对有用信号有效地接收、干扰信号有效地抑制及设备集成化小型化的需求。     

An adaptive integration surface for predicting transonic rotor noise in hovering and forward flights

In this paper, a new permeable adaptive integration surface is developed in order to evaluate transonic rotor noise in accordance with FW-H_pds equations(Ffowcs Williams-Hawkings equations with penetrable data surface). Firstly, a nonlinear near-field solution is computed on the basis of Navier-Stokes equations, which is developed on moving-embedded grid methodology.The solution calculated through the present CFD method is used as the input for acoustic calculations by FW-H_pds equations. Then, two criteria for constructing integration surfaces are established based on the analysis of the quadrupole source strength and the nonlinear characteristic.A new surface is determined adaptively by the pressure gradient or density in a given flowfield,eschewing the uncertainties associated with determining cylinder-shaped integration surfaces. For varying hover cases, transonic noises are simulated with new integration surfaces for a UH-1 model rotor. Furthermore, numerical results of the new integration surface derived from the density perturbation value conform better to experimental data than results derived from the pressure gradient.Finally, the integration surface given by jrqj being 0.1, which is an applicable criterion obtained from hover cases, is used to predict transonic rotor noise in forward flight. The computational accuracy of the new integration surface method has been validated in predicting transonic rotor noise of an AH-1 model rotor at different advance ratios.     

一体化检测系统设计与实现

从工程应用的角度，建立了一体化检测系统模型。系统采用分层设计思想进行工程化设计，注重设计的先进性、灵活性和可靠性。提出了一体化检测系统的设计原则，并对系统中各单元模块进行了详细描述，最后提出了改进和提高可靠性的设想。     

飞机CAD／CAM过程中数据流向的探讨

从回顾南飞公公开展ＣＡＤ／ＣＡＭ工作情况入手，对ＣＡＤ／ＣＡＭ过程中数据流向问题进行了探讨，分析了不足之处，提出了改进数据流向的新思路。     

考虑部件约束的涡扇发动机循环参数分析方法研究

在涡扇发动机初步设计阶段,为了研究部件气动、结构、强度参数对于发动机循环参数求解域的约束,在发动机总体性能稳态计算模型以及尺寸流路计算模型的基础上,利用部件初步设计时采用的Smith图,基于牛顿迭代法构建了一种总体/部件耦合计算方法。在部件主要设计参数的约束边界基础上,采用该方法,能够获取同时满足总体和部件设计要求的循环参数求解域,并进一步获得部件的主要设计参数。使用该方法对第四代双轴混排涡扇发动机EJ200开展了算例验证,获取了部件约束条件下的发动机循环参数求解域,与公布的EJ200数据对比表明,主要部件设计参数误差<4%,表明该方法可以满足工程应用要求。     

雷达-电子战-通信的一体化

为充分发挥武器系统的作战效能，对作战平台上的雷达-电子战-通信一体化技术进行了研究。阐述了雷达与电子战、雷达与通信一体化的必要性和特点，并对一体化的关键技术，如以线性调频与伪随机编码信号的组合为共用信号、共用孔径及其波束控制技术等进行了分析。最后给出了一个采用软件无线电技术的雷达-无线电-通信一体化系统的方案。     

中值定理的应用探讨

通过典型例题，对微分中值定理，积分中值定理在求特殊函数的极限及有关命题，证明等式、不等式方面做了深刻地阐述，探讨怎样正确、理解、应用好中值定理。     

Introduction to global short message communication service of BeiDou-3 navigation satellite system

Short Message Communication (SMC) is a featured service of BeiDou Navigation Satellite System (BDS). After its successful deployment in 2003, Regional Short Message Communication (RSMC) service has been continuously serving China and its neighboring countries and regions, especially in life safety scenarios. In this paper, the architecture of the Global Short Message Communication (GSMC) system is proposed based on the medium earth orbit (MEO) constellation and the crosslinks of the global BeiDou navigation system (BDS-3). Three subtypes of GSMC service, i.e. positioning report, emergency search and rescue (SAR) and regular SMC are designed in accordance with the technical characteristic of integration of navigation and communication in BDS-3, which supports future wide applications of GSMC. The performance of the designed GSMC system is analyzed by numerical calculations. As BDS-3 was officially announced completion on July 31, 2020, GSMC has been providing initial service. First test results of the in orbit GSMC payloads are also presented in the paper to verify the designed capabilities. Preliminary results also show that the requirements of Global Maritime Distress and Safety System (GMDSS) can also be fulfilled.