Design and numerical simulation of a transonic swept fan

CHEN Yong-dang; YANG Hai-cheng; DU Bing-lao

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Design and numerical simulation of a transonic swept fan

更新时间：2026-07-07

- Design and numerical simulation of a transonic swept fan
- Vol. 22, Issue 1, (2007)
- 作者机构：
  
  1. 西北工业大学现代设计与集成制造技术教育部重点实验室,陕西,西安,710072
  2. 中国航天科技集团公司,北京,100037
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2007
- 稿件说明：
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CHEN Yong-dang, YANG Hai-cheng, DU Bing-lao. Design and numerical simulation of a transonic swept fan[J]. 2007, 22(1).
DOI：

CHEN Yong-dang, YANG Hai-cheng, DU Bing-lao. Design and numerical simulation of a transonic swept fan[J]. 2007, 22(1). DOI：

摘要

为实现航空发动机设计知识的集中组织与管理

进行知识组织模型技术研究

提出基于知识本体的知识组织模型构建方法.研究了面向航空发动机设计的知识本体的结构、设计准则、构建方法以及映射技术

并分析了基于本体的知识组织模型的特征

给出了基于知识本体的面向航空发动机设计的知识组织模型的实施框架.此框架对航空发动机设计知识管理的应用研究有参考价值.

Abstract

In order to realize centralized organizing and management for aircraft engine design knowledge

formulation methods of ontology-based knowledge organization model are presented.This paper studies the structure

design criteria

formulation methods and mapping techniques for knowledge ontology for aircraft engine design and analyzes the characteristics of ontology-based knowledge organization model.The implementation framework of ontology-based knowledge organization model for aircraft engine design was given.The research result is of reference value to application research of knowledge management to aircraft engine design.

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Related Author

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LIN Yu-zhen

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LI Ying-hong

CHEN Dong-lin

ZHANG Chi

ZHAO Meng-meng

Related Institution

National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics

The Engineering Institute, Air Force Engineering University

National Key Laboratory on Aero-Engins, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics

School of Jet Propulsion, National Key Laboratory on Aero-Engines, Beijing University of Aeronautics and Astronautics

Engineering College, Air Force Engineering University

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