民机的一种新型布局形式——翼身融合体飞机

 讨论了一种区别于机翼与圆柱机身的传统民机外形——翼身融合体（BWB）外形。从给定容积下减少浸润面积和摩擦阻力的考虑发展出了翼身融合体的概念。在满足系列设计约束条件下讨论了适于大型（800座）客机的翼身融合体的技术和商业上的可能性。概念设计研究表明,翼身融合体外形可获得比常规外形更好的性能。巡航升阻比可从传统外形的19提高至23。480座的BWB外形与同量级的传统外形（A380-700）相比,最大起飞重量可减少18%,每座位燃油消耗可减少32%,具有良好的环保性。通过气动载荷分布规律的反设计,翼型修型和三维优化设计等气动设计方法可以有效减阻和提高BWB的气动性能。由于BWB的高度融合性,讨论了多学科优化设计方法的重要性和有效性。BWB概念能够发展成BWB系列机,进一步提高巡航马赫数也是可能的。     

基于Hamilton-Jacobi方程的编队飞行控制

 针对椭圆参考轨道的编队飞行控制系统,基于哈密尔顿 雅克比（Hamilton-Jacobi）方程,给出一种新的生成函数半解析近似解的计算方法,同时推导了编队飞行控制系统相对运动的线性状态转移矩阵,并且验证了模型的精度。在此基础上,结合一个具体的编队飞行任务,采用线性规划算法得到了队形保持的闭环控制器,该算法得到的是脉冲形式的控制序列,因此更具有实际意义。同时还提出了一种简单的避免生成函数奇异点的方法,从而减少了生成函数间相互转换所带来的计算量。最后的非线性仿真结果验证了控制方法的有效性。     

民机翼身组合体参数化研究

飞机方案设计阶段,迫切需要一个能够快速评估、计算不同参数组合的翼身组合体基本气动力特性的分析平台。为满足这一实际工程设计需要,本文提出运输类飞机参数化概念和具体研究方法,开发了快速分析计算翼身组合体气动力特性分析平台,结合具体算例验证了方法的可行性和工程实用价值。     

承载式车身覆盖件板厚优化及灵敏度分析

探讨了基于有限元模型的承载车身覆盖件板厚优化和灵敏度分析的方法。在大型设计和分析软件UG和ANSYS上建立了车身的有限元模型,分析了覆盖件板厚对车身承载的不同影响效果。     

利用压电驱动器改善飞机横滚性能的试验验证

利用分布粘帖在矩形机翼上下两面的压电驱动器,探索使用该类结构提高飞行器横滚能力的可能性。通过风洞模型设计、材料性能测试、模型固有特性测试、压电柔度矩阵测试等试验项目,保证了有限元模型的计算精度,最终通过模型的风洞试验验证了利用气动弹性效应,获得了附加升力与横滚力矩的方案。该原理性试验说明利用分布式压电驱动器改善横滚性能是可行的。     

Data path synthesis in digital electronics. I. Memory allocation

A data path consists of memory elements (i.e., registers), data operators (i.e. ALUs) and interconnection units (i.e. buses) to control the data transfers in the digital system. Many approaches to hardware allocation for data path synthesis have been proposed in the literature; however, only single-port memory is considered for register allocation and no efficient synthesis approach for multiport memory synthesis. A novel design methodology for data path synthesis using multiport memories is proposed which can be applied to hardware allocation algorithms or to already synthesized data path as a postprocessor to achieve a better design. Illustrations of applying this method to different synthesis examples are presented. Results and improvements over previous techniques are demonstrated. Experiments on benchmarks show very promising results     

Global aerodynamic design optimization based on data dimensionality reduction

In aerodynamic optimization, global optimization methods such as genetic algorithms are preferred in many cases because of their advantage on reaching global optimum. However, for complex problems in which large number of design variables are needed, the computational cost becomes prohibitive, and thus original global optimization strategies are required. To address this need, data dimensionality reduction method is combined with global optimization methods, thus forming a new global optimization system, aiming to improve the efficiency of conventional global optimization. The new optimization system involves applying Proper Orthogonal Decomposition (POD) in dimensionality reduction of design space while maintaining the generality of original design space. Besides, an acceleration approach for samples calculation in surrogate modeling is applied to reduce the computational time while providing sufficient accuracy. The optimizations of a transonic airfoil RAE2822 and the transonic wing ONERA M6 are performed to demonstrate the effectiveness of the proposed new optimization system. In both cases, we manage to reduce the number of design variables from 20 to 10 and from 42 to 20 respectively. The new design optimization system converges faster and it takes 1/3 of the total time of traditional optimization to converge to a better design, thus significantly reducing the overall optimization time and improving the efficiency of conventional global design optimization method.     

Robust space-time adaptive processing for airborne radar in nonhomogeneous clutter environments

Space-time adaptive processing (STAP) holds tremendous potential for the new generation airborne surveillance radar, in which the phased array antennas and pulse Doppler processing mode are adopted. A new STAP approach using the multiple-beam and multiple Doppler channels is presented here for airborne phased array radar. The approach with space-time multiple-beam (STMB) architecture is robust to array errors and has very low system degrees of freedom (DOFs). Hence, it has low sample support requirement and it is very suitable for the practical planar phased array radar under nonhomogeneous clutter environments. Meanwhile, a new nonhomogeneous detector (NHD) based on the correlation dimension (CD) is also proposed here, which is used as an effective method to screen tracing data prior to detection processing. It can further improve the performance of the STAP approach in the severely nonhomogeneous clutter environments. Therefore, a scheme that incorporates the correlation dimension nonhomogeneity detector (CD-NHD) with the STMB is recommended, which we term CD-NHD-STMB. The experimental simulation results indicate that: 1) the STMB processor is robust to array element error and has high performance under nonhomogeneous clutter environments; 2) the CD-NHD is also effective on the nonhomogeneous clutter. As a result, the CD-NHD-STMB scheme is robust to array element error and nonhomogeneous clutter, and therefore available for airborne phased array radar applications.     

机床实体模型复模态空间动位移显示技术的研究

介绍了用实体模型在复模态空间显示机床整机动位移的原理和方法。并在VC++6.0开发平台上用OpenGL语言开发了相应软件。解决了以往同类软件动画效果不能真实地表现实际机床整机的动态位移情况的难题。     

电子束固化高模量纤维增强复合材料力学性能研究

用湿法缠绕工艺制备了M40／EB99—1预浸料，研究了电子束固化高模量石墨化碳纤维M40增强EB99-1环氧树脂复合材料的常规力学性能、耐热疲劳性能和热物理性能，并与M40／5228、M40/4211等热固化复合材料的性能进行了比较。实验研究表明，除了剪切强度稍逊于热固化M40/5228复合材料外，其它常规力学性能都优于热固化M40／5228、M40/211复合材料，表现了较好的综合力学性能。电子束固化M40／EB99—1复合材料经冷热交变循环后的性能明显优于热固化M40／5228、M40/4211复合材料，表现了较好的耐热疲劳性能。