期刊文献+

复杂形式球型收敛调节片喷管内流场计算及分析 被引量:9

Numerical investigation on internal flow of a spherical convergent flap nozzle with complex geometry
下载PDF
导出
摘要 为了分析复杂形式球型收敛调节片喷管(SCFN)三维内流场特性,对六角形和领结形的SCFN进行几何建模,并利用N-S方程和S-A模型,对两种喷管在不同落压比(NPR)下进行了内流场数值模拟.研究表明,计算结果与实验结果吻合较好;在此基础上,对两种喷管的流场特性及性能进行了比较分析. To analyze three-dimensional internal flow characteristic of spherical convergent flap nozzles with hexagonal and bowtie geometries, the geometric models were established and N S equation and S-A model were employed in the numerical simulation. The simulation was developed at different NPR (nozzle pressure ratio). The calculated results are compared favorably well with experimental data. Furthermore, the internal flow characteristic and performance of two nozzles are compared and analyzed.
作者 宋洁 王强
出处 《航空动力学报》 EI CAS CSCD 北大核心 2007年第8期1325-1329,共5页 Journal of Aerospace Power
关键词 航空、航天推进系统 球型收敛调节片喷管 内流场 数值模拟 aerospace propulsion system spherical convergent flap nozzle internal flow field numerical simulation
  • 相关文献

参考文献6

二级参考文献9

  • 1陈懋章.粘性流体动力学基础[M].北京:高等教育出版社,1993..
  • 2[1] Roe P L.Approximate riemann solvers,parameter vect-
  • 3[2] Spalart P R, Allmaras S R. A one-equation turbulence model for aerodynamic flows[R].AIAA 92-0439.
  • 4[3] Venkatakrishnan V. On the accuracy of limiters and
  • 5[4] Hirsch C.Numerical computation of internal and exter-
  • 6[5] Berrier B L, Taylor J G. Internal performance of two nozzle utilizing gimbal concepts for thrust vectoring[R].NASA-TP-2991,1990.
  • 7Carson G T Jr, Caponc F J. Static internal performance of an axisyrmnctric nozzle with multiaxis thrust-vectoring capability[ R] . NASA Technical Memorandum 4237,1991.
  • 8Barth T J, Jespersen D. The design and application of upwind schemes on unstructured meshes[ R]. AIAA 89-0366.
  • 9梁春华,张仁,沈迪刚.国外航空发动机推力矢量喷管技术的发展研究[J].航空发动机,1998,19(1):49-55. 被引量:18

共引文献26

同被引文献65

引证文献9

二级引证文献30

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部