| 基于数值模拟的飞行员高速气流吹袭损伤分析 |
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| 引用本文： | 张朋,田佳林,韩鲁佳,刘洁.基于数值模拟的飞行员高速气流吹袭损伤分析[J].计算物理,2016(2):170-176. |
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| 作者姓名： | 张朋 田佳林 韩鲁佳 刘洁 |
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| 作者单位： | 1. 空军航空大学 航空救生系,吉林 长春,130022;2. 空军航空大学 军事仿真技术研究所,吉林 长春,130022 |
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| 摘 要： | 研究飞行员高速气流吹袭的损伤机理,应用尺度适应模型对人椅系统外流场进行数值模拟.在马赫数为0.6,迎角为-90°~90°条件下的数值计算结果与风洞试验结果吻合较好.对不同马赫数、不同迎角的无防护状态下的人椅系统进行数值模拟,研究发现高速气流吹袭下飞行员面颈部、胸腹部、上臂内侧、小腿迎风侧压力较大;增大人椅系统的迎角可以改善飞行员身体各部分的受力情况.
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| 关 键 词： | 人椅系统 气流吹袭 数值模拟 尺度适应模型 损伤分析 |
CFD Analysis on Pilot??s Injury by Windblast at High Speed |
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| Abstract: | To investigate injury of windblast at high speed, flow around a seat occupant is simulated in a scale adaptive simulation turbulence model. Numerical simulations agree well with wind tunnel experiments at Mach number 0?? 6 and angles of attack from - 90° to 90°. Flow around seat occupant without protection is simulated. Injury of pilot during high speed ejection is investigated. It shows that high pressure zones load on pilot are face, thorax, abdomen, inside of upper arm and windward side of calves. As pitch angle increases pressure distribution on each part can improve. |
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| Keywords: | seat occupant system windblast numerical simulation scale adaptive simulation injury analysis |
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