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尾部喷流对飞行器阻力影响的数值模拟分析 被引量:1
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作者 韩珊珊 冯晓强 +2 位作者 李宏君 全景阁 柳长安 《火箭推进》 CAS 2023年第3期105-114,共10页
底阻在弹类飞行器阻力中占比较大,准确预示底阻对于弹类飞行器飞行性能评估至关重要,而发动机尾部喷流对底阻影响明显。采用基于雷诺平均Navier-Stokes方程的流场仿真方法研究了飞行器底部发动机喷流和外流干扰流场特性,主要分析了喷流... 底阻在弹类飞行器阻力中占比较大,准确预示底阻对于弹类飞行器飞行性能评估至关重要,而发动机尾部喷流对底阻影响明显。采用基于雷诺平均Navier-Stokes方程的流场仿真方法研究了飞行器底部发动机喷流和外流干扰流场特性,主要分析了喷流对飞行器阻力的影响。飞行器安装了两台推力可调的液体火箭发动机,发动机在不同飞行工况下采用不同推力工作。分别研究了亚音速、跨音速和超音速典型飞行工况下弹体底部无喷流状态、单喷管喷流状态和双喷管喷流状态时,飞行器阻力变化情况。结果表明:不同马赫数下,发动机喷流对底部阻力影响情况基本一致,与无喷流情况相比,当发动机工作时,无论单喷管喷流还是双喷管喷流状态,底部发动机喷流引射效应明显,弹体阻力系数明显增加。 展开更多
关键词 底部喷流 双喷管 亚跨超音速 流动干扰 阻力特性
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Characteristic analysis of lock-in for an elastically suspended airfoil in transonic buffet flow 被引量:5
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作者 quan jingge Zhang Weiwei +1 位作者 Gao Chuanqiang Ye Zhengyin 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2016年第1期129-143,共15页
Numerical simulations are performed to study the aeroelastic responses of an elastically suspended airfoil in transonic buffet flow, by coupling the unsteady Reynolds-averaged Navier- Stokes (RANS) equations and str... Numerical simulations are performed to study the aeroelastic responses of an elastically suspended airfoil in transonic buffet flow, by coupling the unsteady Reynolds-averaged Navier- Stokes (RANS) equations and structural motion equation. The current work focuses on the char- acteristic analysis of the lock-in phenomenon. Great attentions are paid to studying the frequency range of lock-in and the effects of the three parameters, namely the structural natural frequency, mass ratio and structural damping, on lock-in characteristic of the elastic system in detail. It is found that when the structural natural frequency is close to the buffet frequency, the coupling fre- quency of the elastic system is no longer equal to the buffet frequency, but keeps the same value as the structural natural frequency. The frequency lock-in occurs and stays present until the structural nature frequency is near the double buffet frequency. It means that the lock-in presents within a broad range, of which the lower threshold is near the buffet frequency, while the upper threshold is near the double buffet frequency. Moreover, the frequency range of lock-in is affected by mass ratio and structural damping. The lower the mass ratio and structural damping are, the wider the range of lock-in will be. The upper threshold of lock-in grows with the mass ratio and structural damping decreasing, but the lower threshold always keeps the same. 展开更多
关键词 Aeroelastic analysisBuffet Elastic airfoil LOCK-IN Transonic flow
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