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| 带偏舵航天飞机的网格生成及流场数值模拟 | |
| 引用本文： | 李盾,纪楚群. 带偏舵航天飞机的网格生成及流场数值模拟[J]. 舰船电子工程, 2005, 25(4): 1-4 |
| 作者姓名： | 李盾 纪楚群 |
| 作者单位： | 北京空气动力研究所,北京,100074 |
| 摘 要： | 以OV-102航天飞机为对象，研究了有舵面偏角的全机单区结构网格的生成方法，模拟并分析了高超声速条件下全机及舵面气动特性。结果表明，带舵偏航天飞机单区结构网格生成方法及流场数值模拟方法，可正确模拟该复杂外形在中小舵偏条件下的气动特性。 |
| 关 键 词： | 结构网格 网格变换 偏舵 数值模拟 |
| 收稿时间： | 2005-03-28 |
| 修稿时间： | 2005-04-11 |
Mesh Generation and Numerical Simulation of Flow Field for OV-102 Space Shuttle with Deflected Rudder |
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| LI Dun,Ji Chuqun. Mesh Generation and Numerical Simulation of Flow Field for OV-102 Space Shuttle with Deflected Rudder[J]. Ship Electronic Engineering, 2005, 25(4): 1-4 | |
| Authors: | LI Dun Ji Chuqun |
| Abstract: | In this paper, the space shuttles OV- 102 with deflected rudder as the object, the method to generate structure mesh of tingle zone is studied. The flow field and aerodynanaic characteristics of space shuttles OV- 102 with deflected rudder are simulated and analyzed at supersonic flow. The result shows that the method to generate structure mesh of single zone can correctly simulate the aerodynamic characteristics with the tail and the rudder complicated configuration. |
| Keywords: | structure mesh mesh generation geometrical transform numerical simulation |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |