| 引用本文: | 杨晓辉,王承尧.飞行器栅格翼三维复杂流场的气动力计算.[J].国防科技大学学报,1996,18(3):1-4.[点击复制] |
| Yang Xiaohui,Wang Chengyao.Calculation of Aerodynamic Forces on the Vehicle and Grid-fins in the Complex Three-dimensional Fluid Field[J].Journal of National University of Defense Technology,1996,18(3):1-4[点击复制] |
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| 飞行器栅格翼三维复杂流场的气动力计算 |
| 杨晓辉, 王承尧 |
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(国防科技大学 航天技术系 湖南 长沙 410073)
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| 摘要: |
| 为了计算作用在飞行器和栅恪翼上的气动力，采用时间相关法数值求解完全气体的三维 Navier-Stokes 方程.并运用通量守恒的分区计算方法，将复杂的飞行器和栅格翼系统分解成八个既相对独立，又相互关联的计算区域，得到了满意的结果。 |
| 关键词: 飞行器，栅恪冀，分区，升力系数，阻力系数，通量守恒 |
| DOI： |
| 投稿日期：1996-03-21 |
| 基金项目: |
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| Calculation of Aerodynamic Forces on the Vehicle and Grid-fins in the Complex Three-dimensional Fluid Field |
| Yang Xiaohui, Wang Chengyao |
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(Department of Aerospace Technology，NUDT，Changsha，410073)
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| Abstract: |
| To calculate the aerodynamic forces on the vehicle and grid-fins，we use time-dependent method to solve the Navier-Stokes equation of ideal gas，and flux conservational multizones method to divide the complex vehicle and grid-fins into eight computational zones which are relatively independent，and correlative with each other at once with satisfactory results. |
| Keywords: vehicle,grid-fins,multizones,lift coefficient,drag coefficient,flux conservation |
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