Title: High precision numerical simulation method for static aeroelastic analysis of wing
Abstract:The coupling between aerodynamic and structure is essential to study static aeroelastic problems.In this paper,the governing equations used for the fluid flow are the three-dimensional Euler equations...The coupling between aerodynamic and structure is essential to study static aeroelastic problems.In this paper,the governing equations used for the fluid flow are the three-dimensional Euler equations,the structural elastic deformation used for a numerical simulation of static aeroelastic for three-dimensional aircraft wing is a finite-element method and the exchanging data of aerodynamic and structure are achieved by a thin plate spline method.The results of computation show that the method developed in this paper is a high precision method and has significant practical value for aircraft design.Read More
Publication Year: 2010
Publication Date: 2010-01-01
Language: en
Type: article
Access and Citation
AI Researcher Chatbot
Get quick answers to your questions about the article from our AI researcher chatbot