| 大攻角侧向喷流流场特性及喷流干扰效应 |
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| 引用本文： | 李立沛,徐敏.大攻角侧向喷流流场特性及喷流干扰效应[J].固体火箭技术,2011,34(5):543-547. |
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| 作者姓名： | 李立沛 徐敏 |
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| 作者单位： | 西北工业大学航天学院,西安,710072 |
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| 基金项目： | 自然科学基金(90816008) |
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| 摘 要： | 采用HLLC近似黎曼解格式求解N-S方程,对大攻角条件下超音速尖拱细长旋成体导弹的单侧向喷流干扰流场进行了数值模拟.并对喷流流场压力分布、喷口附近流动及流场旋涡结构进行了研究,分析了大攻角对细长旋成体侧向喷流干扰压力分布及干扰因子的影响.研究结果表明,HLLC格式计算复杂流场具有较好的数值稳定性；侧向喷流与来流的干扰总...
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| 关 键 词： | 大攻角 侧向喷流 喷流干扰效应:HLLC |
Character and effect of interaction between a lateral jet and supersonic crossflow at large angles of attack |
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| LI Li-pei,XU Min.Character and effect of interaction between a lateral jet and supersonic crossflow at large angles of attack[J].Journal of Solid Rocket Technology,2011,34(5):543-547. |
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| Authors: | LI Li-pei XU Min |
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| Institution: | LI Li-pei,XU Min(College of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China) |
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| Abstract: | The characters of interaction at large angles of attack between a lateral jet and supersonic crossflow over a slender body were simulated numerically.With the solution of a three dimensional full N-S equation which uses the HLLC approximate Riemann solver,the pressure contours of the symmetry plane,the streamlines around the the jet,and the force amplification factor Kf of the jet were described.The results show that HLLC solver has good numerical stability.The interaction reduced the effect of the lateral ... |
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| Keywords: | large angle of attack lateral jet jet interaction HLLC |
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