By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给种基于区域分解算法的可考虑动叶顶部
机匣刮削作用的涡
级计算方法。
By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给种基于区域分解算法的可考虑动叶顶部
机匣刮削作用的涡
级计算方法。
Abstract: By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给种基于区域分解算法的可考虑动叶顶部
机匣刮削作用的涡
级计算方法。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区算法的
动叶顶部间隙和机匣刮削作用的涡
级计算方法。
Abstract: By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区算法的
动叶顶部间隙和机匣刮削作用的涡
级计算方法。
声明:以上例句、词性类均由互联网资源自动生成,部
未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区域分法
考虑动叶顶部间隙和机匣刮削作用
涡
级计
方法。
Abstract: By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区域分法
考虑动叶顶部间隙和机匣刮削作用
涡
级计
方法。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件观点;若发现问题,欢迎向我们指正。
By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区域分解算法的可考虑动叶顶部间隙和机匣刮的涡
级计算方法。
Abstract: By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区域分解算法的可考虑动叶顶部间隙和机匣刮的涡
级计算方法。
声明:以上、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区算法的
动叶顶部间隙和机匣刮削作用的涡
级计算方法。
Abstract: By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区算法的
动叶顶部间隙和机匣刮削作用的涡
级计算方法。
声明:以上例句、词性类均由互联网资源自动生成,部
未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区域法
虑动叶顶部间隙和机匣刮削作用
涡
级计
方法。
Abstract: By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区域法
虑动叶顶部间隙和机匣刮削作用
涡
级计
方法。
声明:以上例句、词性类均由互联网资源自动生成,部
未经过人工审核,其表达内容亦不代表本软件
观点;若发现问题,欢迎向我们指正。
By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种域分解算法的可考虑
部间隙和机匣刮削作用的涡
级计算方法。
Abstract: By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种域分解算法的可考虑
部间隙和机匣刮削作用的涡
级计算方法。
声明:以上例句、词性分类均由互联网资源自生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区域分解法的可考虑动叶顶部间隙和机匣刮削作用的涡
级计
法。
Abstract: By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区域分解法的可考虑动叶顶部间隙和机匣刮削作用的涡
级计
法。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦代表本软件的观点;若发现问题,欢迎向我们指正。
By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区域法
虑动叶顶部间隙和机匣刮削作用
涡
级计
方法。
Abstract: By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出了一种基于区域法
虑动叶顶部间隙和机匣刮削作用
涡
级计
方法。
声明:以上例句、词性类均由互联网资源自动生成,部
未经过人工审核,其表达内容亦不代表本软件
观点;若发现问题,欢迎向我们指正。