期刊文献+
共找到1篇文章
< 1 >
每页显示 20 50 100
Aerodynamic Interpolation for Flight Vehicles with Aerodynamic Axial Asymmetry 被引量:4
1
作者 夏群力 祁载康 《Journal of Beijing Institute of Technology》 EI CAS 1999年第4期430-436,共7页
Aim To study wind tunnel test data interpolation methods for flight vehicle with aerodynamic axial asymmetry. Methods For different body aerodynamic roll angles, proper wind tunnel test schemes were selected and ... Aim To study wind tunnel test data interpolation methods for flight vehicle with aerodynamic axial asymmetry. Methods For different body aerodynamic roll angles, proper wind tunnel test schemes were selected and trigonometric series were used for aerodynamic interpolation. Results and Conclusion A simple and effective scheme for wind tunnel test and an accurate aerodynamic interpolation method are developed with satisfactory results. 展开更多
关键词 aerodynamic interpolation aerodynamic configuration wind tunnel test aerodynamic coefficient
下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部