WANG Jiangfeng
Personal Homepage
Paper Publications
An integrated algorithm for hypersonic fluid-thermal-structural numerical simulation
Hits:

Affiliation of Author(s):航空学院

Journal:MODERN PHYSICS LETTERS B

Key Words:Fluid-structural-thermal aero-heating finite volume method integrated algorithm

Abstract:In this paper, a fluid-structural-thermal integrated method is presented based on finite volume method. A unified integral equations system is developed as the control equations for physical process of aero-heating and structural heat transfer. The whole physical field is discretized by using an up-wind finite volume method. To demonstrate its capability, the numerical simulation of Mach 6.47 flow over stainless steel cylinder shows a good agreement with measured values, and this method dynamically simulates the objective physical processes. Thus, the integrated algorithm proves to be efficient and reliable.

ISSN No.:0217-9849

Translation or Not:no

Date of Publication:2018-05-10

Co-author:Li, Jia-Wei

Correspondence Author:WANG Jiangfeng

Personal information

Professor
Supervisor of Doctorate Candidates

Gender:Male

Alma Mater:南京航空航天大学; Université Pierre et Marie Curie

Education Level:法国巴黎第六大学

Degree:Doctoral Degree in Engineering

School/Department:College of Aerospace Engineering

Discipline:Fluid Mechanics. Fluid Mechanics

Business Address:本部流体楼(C12)- 301室

Contact Information:wangjf@nuaa.edu.cn

Click:

Open time:..

The Last Update Time:..


Copyright©2018- Nanjing University of Aeronautics and Astronautics·Informationization Department(Informationization Technology Center)

MOBILE Version