检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:华耀南[1]
机构地区:[1]中国科学院工程热物理所
出 处:《空气动力学学报》1990年第3期315-320,共6页Acta Aerodynamica Sinica
摘 要:本文用近似因式分解交替方向隐式格式直接求解叶轮机械中原参数三维不可压Euler方程组。在连续方程中引入“拟压缩性”之后,将原来类型不确定的控制方程变成双曲型方程,给定初边值之后用时间推进法求得稳定解,对一个单级压气机转子内部流场进行了计算,结果与实验值比较符合。Using ADI Scheme to solve Euler Equation of primitive variables, the 3D incompressible flowfield in turbomachinery is solved in present paper. After the pseudocompressibility is introduced in the Cotinuity Equation, the system of governing equations is changed from undefined type into hyperbolic type. Giving initial values and boundary conditions, the system of equations can be solved by use of Time-Marching Method to get a stable solution. 3D flowfield within the rotor of the single-stage axial compressor at the Pennsylvania State University is calculated in present paper. The prediction results quite agree with experimental data.
分 类 号:V231.3[航空宇航科学与技术—航空宇航推进理论与工程]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:216.73.216.15