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计算机系统应用英文版:2013,22(2):53-56,79

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飞机结构静力试验CAD系统

侯同济, 张建锋, 滕申科

(中国飞机强度研究所, 西安 710065)

CAD System for Aircraft Structure Static Test Design

HOU Tong-Ji, ZHANG Jian-Feng, TENG Shen-Ke

(Aircraft Strength Research Institute of China, Xi’an 710065, China)

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本文已被：浏览 1471次下载 2868次
Received:June 21, 2012 Revised:August 21, 2012

中文摘要: 飞机结构静力试验设计系统(Aircraft Structure Static Test Design System-ASSTDS)是用于全尺寸飞机结构静力试验设计的、图形交互式的计算机辅助设计(CAD)软件系统. 本文介绍了基于面向对象技术完成的软件系统需求分析、功能分解和对象抽象, 软件开发过程中建立的系统对象体系以及主要对象和它们之间的相互关系. 飞机结构静力试验设计系统采用VC++编程语言在Windows操作系统上开发完成的.

中文关键词: 静力试验辅助设计面向对象

Abstract:The ASSTDS system is a special graphical interactive CAD software for the aircraft structure static test design. The paper introduces the requesting analysis, function decomposing and object abstracting for the sofeware based on object-oriented technology and the object architecture in the software development. The main objects and their relationships are also described. ASSTDS is developed in the programming language VC++ on the Windows operation system.

keywords: static test CAD object-oriented

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Author Name	Affiliation
HOU Tong-Ji	Aircraft Strength Research Institute of China, Xi’an 710065, China
ZHANG Jian-Feng	Aircraft Strength Research Institute of China, Xi’an 710065, China
TENG Shen-Ke	Aircraft Strength Research Institute of China, Xi’an 710065, China

Author Name	Affiliation
HOU Tong-Ji	Aircraft Strength Research Institute of China, Xi’an 710065, China
ZHANG Jian-Feng	Aircraft Strength Research Institute of China, Xi’an 710065, China
TENG Shen-Ke	Aircraft Strength Research Institute of China, Xi’an 710065, China

引用文本：
侯同济,张建锋,滕申科.飞机结构静力试验CAD系统.计算机系统应用,2013,22(2):53-56,79
HOU Tong-Ji,ZHANG Jian-Feng,TENG Shen-Ke.CAD System for Aircraft Structure Static Test Design.COMPUTER SYSTEMS APPLICATIONS,2013,22(2):53-56,79