学术
国际标准刊号：ISSN 1000-0879
国内统一刊号：CN 11-2064
摘 要:
介绍了燃气作动简气动模拟加载装置设计思路和原理，并阐述了利用斜面上升法进行模拟加载装置设计的计算方法．实践应用表明气动模拟加载装置方案基本能够真实、等效的模拟弹翼气动载荷，利用该装置大大地缩短研制周期、节省研制经费，可以进行推广应用．[著者文摘]
文章出处:
《力学与实践》-2008年30卷1期,40 -41-43,40页
Mechanics and Engineering
栏目信息:
[参考文献]
DESIGN AND APPLICATION STUDY ON THE SIMULATION LOAD DEVICE FOR AERODYNAMIC LOADS OF MISSILE WINGS
CAI Wanhua, HE Xinsuo, REN Hua（School of Mechanics, Civil Eng ＆ Architecture, Northwestern Polytechnical University, Xi＇an 710072, China;No. 210 Institute, the Second Academy of CASIC, Xi＇an 710065, China）
Abstract:
This paper disscusses the design principle of the gas actuator used as the aerodynamic simulation load device, and the calculation of the aerodynamic simulation load by using the inclined plane and ascending method. It is shown that the scheme of the aerodynamic simulation load device is practicable; the aerodynamic loads of missile wings can be simulated in a practical and equivalent way, which may greatly reduce the time and expense for related development.[著者文摘]
Key words:
missile wing, aerodynamic simulation, loading structure
基金资助:
国家自然科学基金（10672133）项目资助.
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