摘要
介绍了一种飞机综合设计与评估技术的基础平台,包括使用的技术参数,软件功能,数学模型,设计结果,和8m×6m风洞试验结果、资料值进行的比较等。该平台构思科学、功能齐备、界面友好、拓展性强,设计结果可靠,是飞机设计师和气动布局研究人员的实用工具。
A base code for aircraft synthetic design and evaluation is presented, including the technical parameters, the code functions, the mathematical model, the design results, and the comparison of designed results with 8 m × 6 m WT testing and information data. It can be said that the code is a useful tool for the aircraft designer and aerodynamic configuration researchers due to the code's scientific method, universal functions, friend interface, wide-extension and reliable design data.
出处
《流体力学实验与测量》
EI
CSCD
北大核心
2004年第2期6-10,共5页
Experiments and Measurements in Fluid Mechanics
关键词
飞机设计
评估技术
气动布局
数学模型
code
technical parameter
functions
mathematical model
computational example
results comparison
