| 多重网格方法及其在高超声速进气道中的应用 |
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| 引用本文： | 尹凤娥.多重网格方法及其在高超声速进气道中的应用[J].航空计算技术,2010,40(2):32-36. |
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| 作者姓名： | 尹凤娥 |
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| 作者单位： | 中南林业科技大学,土木工程与力学学院,湖南,长沙,410004 |
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| 摘 要： | 随着计算流体力学的发展，多重网格在求解欧拉方程、N—S方程过程中得到了广泛应用。将这种方法应用于高超声速进气道的数值模拟中，通过具体的算例，验证了该方法的有效性。
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| 关 键 词： | 多重网格 高超声速 有限体积法 |
Applications of Multi-grid Scheme in the Hypersonic Inlet |
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| YIN Feng-e.Applications of Multi-grid Scheme in the Hypersonic Inlet[J].Aeronautical Computer Technique,2010,40(2):32-36. |
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| Authors: | YIN Feng-e |
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| Institution: | YIN Feng-e ( School of Civil Engineering and Mechanics, Central South University of Forestry and Technology, Changsha 410004, China) |
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| Abstract: | With the development of computer technology and fluid dynamics, multi- grid scheme has been widely used in solving Euler equations and Navier- Stokes equations. In this thesis, I research the possibility of using the method to optimize the numerical simulation of hypersonic inlet. Some practical examples of simulation results show that the method has good validity and potential to practical application. |
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| Keywords: | multi- grid hypersonic finite volume method |
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