| 1. | If this load centroid is behind the elastic axis of the wing structure, then a nose-down twist of the main wing surface results .
如果该载荷重心在机翼结构弹性轴之后，则引起主机翼表面前端向下的扭转。 |
| 2. | Layout optimization of aircraft wing with topology shaping sizing variables all considered
基于杂交算法的机翼结构布局优化设计 |
| 3. | Multi - objective optimization design of wing structure with the model management framework
基于模型管理框架的机翼结构多目标优化设计 |
| 4. | Tailless flying wing aerodynamic configuration being optimal selection in ucav general layout design
大展弦比复合材料机翼结构建模与气动弹性分析 |
| 5. | The frame - change law of space - time and the response functionals of simple materials with internal constraints
基于仿生的大展弦比机翼结构布局形式研究 |
| 6. | In order to affirm that our ideal and project of lab ' s establishment are right , we then introduce an example about lab ' s establishment , which is about remote real - time health monitoring system for structure of an aeromodelling ' s wing
为了验证我们建立实验室的框架和方案是行得通的，文章接着又研究了采用一架航模飞机作为研究对象，来建立一套监控航模飞机机翼结构的健康监控系统。 |
| 7. | The optimization results of three simple examples and wing of global hawk show that this method has good generalization and has the ability to find good optimal solutions and it can be used in mdo conveniently , so it has great practical value in engineering design
三个简单算例以及全球鹰机翼结构形状优化结果表明这种方法思路清晰，通用性较好，并具有较好的优化效果，适合用在mdo中。 |
| 8. | Although aircraft designers and engineers continued to employ wing - warping techniques for years afterward ( especially on early monoplanes such as the bleriot xi ) , ever faster flight speeds eventually led them to beef up wing structures to resist the resulting stresses
虽然其后许多年间，飞机设计师和工程师仍继续采用翘曲机翼设计（尤其是布雷修xi型等早期单翼机） ，但由于飞行速度不断提升，终于迫使他们加强机翼结构，以承担所增加的应力。 |
| 9. | So , when we get the dates of stress and distortion of wing ' s model structure , which have been calculated by computer , we can simulate the dates of the real wing ' s structure , which we will get through stress sensors and distortion sensors . when we transmit those dates to the center computer through remote wireless transmission devices , the computer will analyze those dates according as scientific fault criterion . so we can carry out the remote real - time health monitoring for wing ' s structure
这样，我们读取计算出的机翼结构模型在受力时的应力、变形值就可以模拟出在采用实体机翼作为研究对象时应力、变形传感器传回的数据，把这些数据通过远程无线数据传输设备传到数据处理计算机上采用科学的故障判据对这些数据进行处理就可以实现对机翼结构的实时远程健康监控。 |
| 10. | At last , considering the practical application , the preceding contents have been integrated altogether as a soft system in this paper and the design objective of the composite synthesis optimization for aircraft structures have been realized through the multilevel hybrid optimization model when a specific application of the forward - wing design has been tested
最后本文从工程实际应用角度考虑，把上述内容通过一个具体的前掠机翼结构设计问题集成为一个软件系统，通过多级混合优化模型，实现了本文提出的复合材料飞机结构的综合优化设计目标。 |
