A coupled Navier-Stokes/free-wake method is developed to predict the rotor aerodynamics and wake.The widely-used Farassat 1 Aformulation is adopted to predict the rotor noise.In the coupled method,the Reynolds-average...A coupled Navier-Stokes/free-wake method is developed to predict the rotor aerodynamics and wake.The widely-used Farassat 1 Aformulation is adopted to predict the rotor noise.In the coupled method,the Reynolds-averaged Navier-Stokes(RANS)solver is established to simulate complex aerodynamic phenomena around blade and the tip-wake is captured by a free-wake model without numerical dissipation in the off-body wake zone.To overcome the time-consuming of the coupling strategy in previous studies,a more efficient coupling strategy is presented,by which only the induced velocity on the outer boundary grid need to be calculated.In order to obtain blade control settings,a delta trimming procedure is developed,which is more efficient than traditional trim method in the calculation of Jacobian matrix.Several flight conditions are simulated to demonstrate the validity of the coupled method.Then the rotor noise of operational load survey(OLS)is studied by the developed method as an application and the computational results are shown to be in good agreements with the available experimental data.展开更多
根据散货船特点探讨了一种面向工程应用的船舶自由浮态计算简化方法.在矩阵法的基础上,将7个水线面要素简化到4个,简化雅克比矩阵求解.采用全选主元高斯消去法求解线性方程组,以船舶浮态平衡方程组作为迭代终止条件,保证计算精度.以散货...根据散货船特点探讨了一种面向工程应用的船舶自由浮态计算简化方法.在矩阵法的基础上,将7个水线面要素简化到4个,简化雅克比矩阵求解.采用全选主元高斯消去法求解线性方程组,以船舶浮态平衡方程组作为迭代终止条件,保证计算精度.以散货船"DOLCE VITA"及"RUI AN CHENG"为例进行了实例计算,对20个压载舱进行了20万次随机装载实验,验证了算法在有横倾下的收敛性和稳定性;对5个货舱进行了20万次随机装载实验,验证了算法在有纵倾下的收敛性和稳定性;对典型载况进行计算,和装载手册给定值相比,吃水差误差都在0.01m以下.结果表明:该算法只需计算任意倾斜水线面下的排水体积和浮心坐标,计算量较小,程序实现简单,实时性、鲁棒性较好,具有一定的工程实用价值.展开更多
针对典型跨声速民用客机的机翼/机身/平尾构型开展了基于离散伴随技术的气动外形优化设计方法研究,并采用自由型面变形(FFD)技术在优化设计过程中进行平尾的整体偏转,以实现最终设计结果全机俯仰力矩配平。采用基于雷诺平均Navier-Stoke...针对典型跨声速民用客机的机翼/机身/平尾构型开展了基于离散伴随技术的气动外形优化设计方法研究,并采用自由型面变形(FFD)技术在优化设计过程中进行平尾的整体偏转,以实现最终设计结果全机俯仰力矩配平。采用基于雷诺平均Navier-Stokes(RANS)方程的离散伴随技术求解气动参数对设计变量的梯度,使梯度求解计算量与设计变量个数实现解耦,提高了优化效率。应用FFD技术对全机构型进行整体参数化,可通过FFD控制体控制机翼外形的变化以及平尾偏转,在实现机翼优化设计的同时通过偏转平尾来进行力矩配平,避免了单独优化机翼外形可能带来的额外配平阻力。采用序列二次规划算法进行基于梯度的优化设计并处理大规模的约束条件。以Drag Prediction Workshop IV Common Research Model作为初始构型进行了有/无力矩配平约束的优化设计,并在优化过程中施加升力约束以及几何约束。算例结果表明,优化后的气动外形显著改善了机翼表面压力分布,消除了激波,在力矩配平约束下的算例中,通过平尾的偏转实现了俯仰力矩配平下的机翼优化设计。展开更多
文摘A coupled Navier-Stokes/free-wake method is developed to predict the rotor aerodynamics and wake.The widely-used Farassat 1 Aformulation is adopted to predict the rotor noise.In the coupled method,the Reynolds-averaged Navier-Stokes(RANS)solver is established to simulate complex aerodynamic phenomena around blade and the tip-wake is captured by a free-wake model without numerical dissipation in the off-body wake zone.To overcome the time-consuming of the coupling strategy in previous studies,a more efficient coupling strategy is presented,by which only the induced velocity on the outer boundary grid need to be calculated.In order to obtain blade control settings,a delta trimming procedure is developed,which is more efficient than traditional trim method in the calculation of Jacobian matrix.Several flight conditions are simulated to demonstrate the validity of the coupled method.Then the rotor noise of operational load survey(OLS)is studied by the developed method as an application and the computational results are shown to be in good agreements with the available experimental data.
文摘根据散货船特点探讨了一种面向工程应用的船舶自由浮态计算简化方法.在矩阵法的基础上,将7个水线面要素简化到4个,简化雅克比矩阵求解.采用全选主元高斯消去法求解线性方程组,以船舶浮态平衡方程组作为迭代终止条件,保证计算精度.以散货船"DOLCE VITA"及"RUI AN CHENG"为例进行了实例计算,对20个压载舱进行了20万次随机装载实验,验证了算法在有横倾下的收敛性和稳定性;对5个货舱进行了20万次随机装载实验,验证了算法在有纵倾下的收敛性和稳定性;对典型载况进行计算,和装载手册给定值相比,吃水差误差都在0.01m以下.结果表明:该算法只需计算任意倾斜水线面下的排水体积和浮心坐标,计算量较小,程序实现简单,实时性、鲁棒性较好,具有一定的工程实用价值.
文摘针对典型跨声速民用客机的机翼/机身/平尾构型开展了基于离散伴随技术的气动外形优化设计方法研究,并采用自由型面变形(FFD)技术在优化设计过程中进行平尾的整体偏转,以实现最终设计结果全机俯仰力矩配平。采用基于雷诺平均Navier-Stokes(RANS)方程的离散伴随技术求解气动参数对设计变量的梯度,使梯度求解计算量与设计变量个数实现解耦,提高了优化效率。应用FFD技术对全机构型进行整体参数化,可通过FFD控制体控制机翼外形的变化以及平尾偏转,在实现机翼优化设计的同时通过偏转平尾来进行力矩配平,避免了单独优化机翼外形可能带来的额外配平阻力。采用序列二次规划算法进行基于梯度的优化设计并处理大规模的约束条件。以Drag Prediction Workshop IV Common Research Model作为初始构型进行了有/无力矩配平约束的优化设计,并在优化过程中施加升力约束以及几何约束。算例结果表明,优化后的气动外形显著改善了机翼表面压力分布,消除了激波,在力矩配平约束下的算例中,通过平尾的偏转实现了俯仰力矩配平下的机翼优化设计。
