关键词:固体推进剂火箭发动机;喷管;计算机辅助设计;流场;烧蚀;有限元法中图分类号:V435文献标识码:ATheintegrateddesignandanalysisofsolidrocketmo-tornozzlesBAOFu-ting,GUODa- ing,ZHAOFei,LIUJun-ping!Co egeofAstronauticsofNorthwesternPo ytechnica University,Xi'an710072,China.Abstract:Theconfigurationofso id...
Solid_Rocket_Motor_Analysis妄想**想i 上传503.76 KB 文件格式 zip 《固体火箭发动机分析》是一项针对小型铝-冰固体火箭发动机性能的解析性模拟研究。该研究通过建立数学模型,考虑了固体火箭燃料的特性、推进剂组分以及发动机结构参数等因素,对铝-冰固体火箭发动机的性能进行了全面分析。研究内容涵盖了推进剂燃烧特性、...
dymamiccharacteristicsanalysisofsolidrocketmotormagneticsuspensiontest 系统标签: 磁悬浮发动机dymamicsuspension火箭rocket 书文章编号:1006-2793(2005)01-0072-03固体火箭发动机磁悬浮试验架系统动态性能分析!王利娜1,赵建辉2(1.中国航天科技集团公司四院四〇一所,西安710025;2.空军工程大学工程学院,西安710038)摘要:在磁悬...
Bala Krishna, B Siva Prasad, "Design & Analysis of Solid Rocket Motor Casing for Aerospace Applications", International Journal of Current Engineering and Technology, Volume 5,No. 3, June 2015, pp. 1947-1954.P. Mahesh Babu, G. Bala Krishna and B Siva Prasad, "Design & Analysis of Solid...
In this paper, the modal analysis of a solid rocket motor under a certain constraint condition is analyzed by using the finite element software ANSYS. It utilizes the dynamic characteristics to appraise and provides for further research on structural improve and design work in the solid rocket ...
Modeling of solid rocket motor components and its assembly is done in CATIAV5R19. Stress distributions are due to the effect of working stress developed in the components. The maximum working stress is compared with allowable yield stress of the material. Final conclusion brings out a well ...
The basis for a three-dimensional finite element acoustic analysis computer code to be used on the combustion instability analysis of solid rocket motor ca... hackett,robert m 被引量: 1发表: 1975年 固体火箭发动机燃烧室过载下的三维应力分析 Three-dimensional stress analysis in solid rocket motor ...
A multidimensional implicit Navier-Stokes analysis that uses numerical solution of the ensemble-averaged Navier-Stokes equations in a nonorthogonal, body-fitted, cylindrical coordinate system has been applied to the simulation of the steady mean flow in solid propellant rocket motor chambers. The calculat...
Response surface method(RSM) is an effective technique to cut down the high computational cost of solid rocket motor(SRM) interior ballistic models,and the key problem in application of RSM is how to choose an appropriate fit functions.In the paper,the main response surface methods are explicate...
弯曲载荷作用下固体火箭发动机裙端连接螺孔受力分析 force analysis of joint bolt holes in solid rocket motor skirt subjected to be 下载积分:2000 内容提示: 第34卷第3期固体火箭技术of Sol i d R0cketTechnol og) rJ oum alV01.34 N o.3 20l l弯曲载荷作用下固体火箭发动机裙端连接螺孑L受力分析①...