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| 大迎角翼—身组合体涡流特性计算 | |
| 引用本文： | 熊善文 吴小勇. 大迎角翼—身组合体涡流特性计算[J]. 空气动力学学报, 1997, 15(1): 102-107 |
| 作者姓名： | 熊善文 吴小勇 |
| 作者单位： | 北京航空航天大学!北京，100083 |
| 摘 要： | 论述了用非线性离散涡法来模拟大迎角下翼－身组合体涡流绕流的计算模型及计算方法；给出了一个典型翼－身组合体的涡流流态计算结果及非线性气动特性和截面压强分布。 |
| 关 键 词： | 翼－身组合体 大迎角 离散涡法 |
Calculation of Vortex Flow Characteristics on Wing-Body Combination at High Angles of Attack |
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| Xiong Shanwen, Wu Xiaoyong, Feng Yanan. Calculation of Vortex Flow Characteristics on Wing-Body Combination at High Angles of Attack[J]. Acta Aerodynamica Sinica, 1997, 15(1): 102-107 | |
| Authors: | Xiong Shanwen Wu Xiaoyong Feng Yanan |
| Abstract: | Two computed models and a numerical method based on nonlinear discrete vortex method are presented to simulate the vortex flow about wing-body combinations.The two computed models consist of a same fuselage vortex model but a different vortex model for simulating the wing leading-edge vortex indiyidually, one model has a concentrated line vortex/sink and the other has a number of diffused vortex filaments. The vortex flow patterns and the nonlinear aerodynamic characteristics of a typical wing-body combination haye been calculated. Comparing with the experimental data, it is shown that the computational results are resonably accurate. |
| Keywords: | wing-body combination high angles of attack discrete vortex method |
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