aircraft wing

Vibration Test and Identification of Modal Parameter of Aircraft Wing Model

机翼模型振动试验的模态参数识别

Method of Aircraft Wing Structural Weight Evaluation Based on FSD & FEM

基于满应力优化与有限元分析的机翼结构重量估算法

Study of the Mass Estimation and Prediction Method for Aircraft Wing Parts

飞机机翼结构质量分配方法研究

Analysis and Synthesis Based Aircraft Wing Structural Layout Study

飞机翼面结构布局综合设计方法研究

Structural Layout Optimization Method of Aircraft Wing Based on Ant Colony Algorithm

基于蚁群算法的机翼结构布局优化方法

Research on Load Distribution of Aircraft Wing / Fuselage Main Joints

某型飞机翼身主接头的载荷分配研究

Aircraft wing structural layout study based on hierarchy optimization

基于分级优化的飞机翼面结构布局综合技术研究

Using VBA to Design an Aircraft Wing Surface Based on CATIA Software

基于CATIA软件对VBA的支持进行飞机翼面的造型设计

A new kind of modelling was proposed on aircraft wing structural analysis and optimization .

提出一种新的飞机翼面结构分析和优化的建模技术。

Research on Aircraft Wing Typical Structural Parts Library Based on The Knowledge of Structural Parts Features

基于特征知识的飞机翼类典型结构件库研究

The Application of Finite Element Method in the Forming of Aircraft Wing Skin Panels

有限元法在机翼整体壁板成形中的应用

Application of BP Neural Networks Based on Bayesian Regularization to Aircraft Wing Loads Analysis

贝叶斯正则化BP网络在机翼载荷分析中的应用

The second half of the paper presents the research of the layout optimization of aircraft wing .

后半部分利用近似技术对飞机机翼前梁布局优化进行了研究。

Finally , a certain kind of aircraft wing is used as example to examine the algorithm .

以某型飞机机翼为例验证算法的有效性。

An Updated Multi-objective Genetic Algorithm and Its Application to Unmanned Aircraft Wing Structural Optimization

改进的多目标遗传算法在无人机机翼结构优化中的应用

To test this algorithm , one design example , one rib of an aircraft wing , is given .

为验证该算法，给出了一个飞机水平安定面翼肋设计实例。

Fatigue life prediction of an aircraft wing

某机翼疲劳寿命估算

Intelligent control of electrohydraulic servo loading system for variable-sweep aircraft wing

变后掠机翼电液伺服加载系统的智能控制

This thesis brings forwards a civil aircraft wing design process based on artificial neural network technology and database technology .

本文以人工神经网络技术和数据库技术为基础，建立了一套基于人工神经网络方法的民用飞机先进气动力机翼设计流程。

Geometrical Optimization of Aircraft Wing Based on double-state technology

基于两相法的机翼结构几何优化设计

Ensuring the stability of the composite skin is of great significance in the design of aircraft wing structures .

复合材料蒙皮稳定性是飞机翼面结构设计需要考虑的重要方面。

This paper presents a novel algorithm , which aims at the solution of geometrical optimization for aircraft wing .

针对机翼结构的几何优化问题，提出了一种基于两相法的几何优化设计新方法。

Structural Layout Optimization of Aircraft Wing under Aeroelastic Constrains

考虑气动弹性约束的机翼结构布局优化设计

A practical aircraft wing is utilized as an example and the optimal results show that the proposed method is feasible .

以国外某飞机机翼为例，结果表明本文提出分级优化的思路与所采用的集成方法是可行的，并且具有很好的数值效果。

A Method for Calculating Anti-Bird Impact Capability of an Aircraft Wing Using ANSYS / LS-DYNA Software

基于ANSYS/LS-DYNA的飞机机翼前缘抗鸟撞分析

Active flutter suppression is one of the mainstream methods about flutter suppression for aircraft wing .

颤振主动控制是目前抑制机翼颤振的主流方法。

In the design of aircraft wing structure , the structure of lightweight has always been one of the main goals of design .

在飞行器翼翅结构的设计中，结构的轻量化一直是设计的主要目标之一。

Some suggestions are also given here on the problems or research directions of the composite main joints of aircraft wing structure .

并针对翼面结构复合材料主承力接头存在的问题和研制方向表明了看法。

Making aircraft wing vary under different flying speeds is a key technology of variable camber adaptive wing .

实现机翼在不同的飞行状态下的最优气动外形是变弯度自适应机翼的一项关键技术。

Describes the assembly information of aircraft wing using Object-Oriented method , and establishes a uniform wing assembly hierarchical tree structure .

采用面向对象技术描述机翼装配信息，建立了统一的机翼装配阶层结构树。