![]() |
个人信息Personal Information
教授 博士生导师
招生学科专业:
力学 -- 【招收博士、硕士研究生】 -- 航空学院
航空宇航科学与技术 -- 【招收硕士研究生】 -- 航空学院
机械 -- 【招收博士、硕士研究生】 -- 航空学院
主要任职:飞行器流体物理全国重点实验室学术委员会委员,中国振动工程学会理事,中国航空学会变体飞行器分会、中国振动工程学会模态分析与试验专委会、非线性振动专委会等四个专业委员会副主任委员/委员
其他任职:SCI期刊《Acta Mechanica Sinica》期刊责任编辑、《力学进展》、《振动工程学报》、《力学学报》和《动力学与控制》等四种期刊的青年编委
性别:男
毕业院校:Nanjing University of Aeronautics and Astronautics
学历:南京航空航天大学
学位:工学博士学位
所在单位:航空学院
联系方式:ruihwang@nuaa.edu.cn
Reduced-Order Modeling of Unsteady Hypersonic Aerodynamics in Multi-Dimensional Parametric Space
点击次数:
所属单位:航空学院
发表刊物:JOURNAL OF APPLIED FLUID MECHANICS
关键字:Reduced order model Proper orthogonal decomposition Kriging surrogate Piston theory Multi-dimensional parametric space
摘要:A novel reduced order model (ROM) for unsteady hypersonic aerodynamics is developed, which is applicable for the variations of multi-parameters. The key to the developed ROM lies in the CFD-based model reduction of the steady aerodynamic component, which stems from the quasi-steady nature of aerodynamic forces in the hypersonic regime. Concretely, the proper orthogonal decomposition (POD) method, combined with Kriging interpolation, is used to construct the ROM for the steady aerodynamic component; meanwhile the unsteady part is directly obtained from Donov's third-order piston theory. The new procedure is applied to a three-dimensional low aspect ratio wing (Lockheed F-104 Starfighter wing). It is shown that the developed ROM is able to accurately predict the unsteady hypersonic aerodynamic loads over a wide range of different flight conditions compared with the direct CFD computation.
ISSN号:1735-3572
是否译文:否
发表时间:2018-07-01
合写作者:陈志强
通讯作者:黄锐