针对新能源无人机高空低速长航时的特点,开展对低雷诺数翼型气动性能优化研究。以带精英策略的非支配排序的遗传算法(NSGA-II)为优化算法,并采用CST(Class Function/Shape Function Transformation)翼型参数化方法,对低雷诺数翼型的多...针对新能源无人机高空低速长航时的特点,开展对低雷诺数翼型气动性能优化研究。以带精英策略的非支配排序的遗传算法(NSGA-II)为优化算法,并采用CST(Class Function/Shape Function Transformation)翼型参数化方法,对低雷诺数翼型的多目标优化进行探讨。经过对AH79-100B翼型进行效率因子和俯仰力矩系数的多目标优化,结果是翼型的效率因子变化较小,但作为主要优化目标的俯仰力矩系数则有明显下降,成功降为优化前翼型的89%。这说明了该气动优化方法在低雷诺数环境下的有效性,为低雷诺数翼型的设计及优化提供参考。展开更多
Variable-camber technology is considered an effective way to adaptively improve the aerodynamic performance of aircraft under various flight conditions.This paper studies the aerodynamic characteristics of the trailin...Variable-camber technology is considered an effective way to adaptively improve the aerodynamic performance of aircraft under various flight conditions.This paper studies the aerodynamic characteristics of the trailing-edge variable-camber technology by means of Computational Fluid Dynamics(CFD)and a drag decomposition method.Trailing-edge variable-camber technology can be simply realized by the continuous deflection of the flaps and ailerons of a wing.A supercritical airfoil is used to study the two-dimensional effect of variable-camber technology,and a wide-body airplane model is used to validate the three-dimensional improvement in the wing’s airfoil made by variable-camber technology.An optimization strategy for airfoil that incorporates variable-camber technology is proposed.The optimization results demonstrate that the proposed method can obtain better results than the traditional segregated shape optimization.展开更多
针对含有内部金属障碍物的开孔屏蔽腔体的结构特点,采用扩展的传输线方法理论,建立了平面波照射下腔体电场屏蔽效能的等效电路模型,推导了近似计算解析式,并计算分析了内部金属障碍物对开孔腔体屏蔽效能的影响,分析了障碍物跨度、到腔...针对含有内部金属障碍物的开孔屏蔽腔体的结构特点,采用扩展的传输线方法理论,建立了平面波照射下腔体电场屏蔽效能的等效电路模型,推导了近似计算解析式,并计算分析了内部金属障碍物对开孔腔体屏蔽效能的影响,分析了障碍物跨度、到腔体开孔缝面的距离和障碍物开缝距离对腔体电场屏蔽效能的影响.在0～1 GHz范围内,利用传输线方法（transmission line method,TLM）计算了含内部障碍物腔体屏蔽效能,与CST软件仿真结果验证了本方法的有效性.计算结果表明：内部金属障碍物提高了腔体的屏蔽效能,改变了腔体的谐振频率,且障碍物尺寸越大对腔体影响越大;障碍物距离开缝面越远、跨度越大、障碍物开缝距离越近,腔体屏蔽效能越大.展开更多
文摘针对新能源无人机高空低速长航时的特点,开展对低雷诺数翼型气动性能优化研究。以带精英策略的非支配排序的遗传算法(NSGA-II)为优化算法,并采用CST(Class Function/Shape Function Transformation)翼型参数化方法,对低雷诺数翼型的多目标优化进行探讨。经过对AH79-100B翼型进行效率因子和俯仰力矩系数的多目标优化,结果是翼型的效率因子变化较小,但作为主要优化目标的俯仰力矩系数则有明显下降,成功降为优化前翼型的89%。这说明了该气动优化方法在低雷诺数环境下的有效性,为低雷诺数翼型的设计及优化提供参考。
基金supported by the National Natural Science Foundation of China(Nos.11872230 and 91852108)。
文摘Variable-camber technology is considered an effective way to adaptively improve the aerodynamic performance of aircraft under various flight conditions.This paper studies the aerodynamic characteristics of the trailing-edge variable-camber technology by means of Computational Fluid Dynamics(CFD)and a drag decomposition method.Trailing-edge variable-camber technology can be simply realized by the continuous deflection of the flaps and ailerons of a wing.A supercritical airfoil is used to study the two-dimensional effect of variable-camber technology,and a wide-body airplane model is used to validate the three-dimensional improvement in the wing’s airfoil made by variable-camber technology.An optimization strategy for airfoil that incorporates variable-camber technology is proposed.The optimization results demonstrate that the proposed method can obtain better results than the traditional segregated shape optimization.
文摘针对含有内部金属障碍物的开孔屏蔽腔体的结构特点,采用扩展的传输线方法理论,建立了平面波照射下腔体电场屏蔽效能的等效电路模型,推导了近似计算解析式,并计算分析了内部金属障碍物对开孔腔体屏蔽效能的影响,分析了障碍物跨度、到腔体开孔缝面的距离和障碍物开缝距离对腔体电场屏蔽效能的影响.在0～1 GHz范围内,利用传输线方法（transmission line method,TLM）计算了含内部障碍物腔体屏蔽效能,与CST软件仿真结果验证了本方法的有效性.计算结果表明：内部金属障碍物提高了腔体的屏蔽效能,改变了腔体的谐振频率,且障碍物尺寸越大对腔体影响越大;障碍物距离开缝面越远、跨度越大、障碍物开缝距离越近,腔体屏蔽效能越大.
