{"title":"Bayesian inference of airfoil icing condition from simulated ice shapes","authors":"Xinyu Zhong, Zifei Yin, Weiliang Kong, Hong Liu","doi":"10.1007/s42401-024-00281-6","DOIUrl":null,"url":null,"abstract":"<div><p>Motivated by the difficulty of accurately determining the inflow parameters in icing wind tunnels and flight tests, the Markov Chain Monte Carlo (MCMC) method, a commonly used Bayesian inference method, is explored to solve the inverse problem with the help of an icing software. The icing software, SJTUICE, is used to produce ice shapes for inversion and serves as the prediction tool in the iterations of the inversion problem. The influence of prior estimation of different icing parameters on the convergence and accuracy of the inversion problem is discussed. The feasibility of the MCMC method in inferring the inflow condition in terms of rime ice and glaze ice is assessed. Generally, fast convergence and good accuracy in terms of single inflow parameter inversion can be easily achieved. However, the number of iterations required increases rapidly with the number of inflow parameters in the MCMC method.</p></div>","PeriodicalId":36309,"journal":{"name":"Aerospace Systems","volume":"8 2","pages":"369 - 381"},"PeriodicalIF":0.0000,"publicationDate":"2024-03-21","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Systems","FirstCategoryId":"1085","ListUrlMain":"https://link.springer.com/article/10.1007/s42401-024-00281-6","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"Earth and Planetary Sciences","Score":null,"Total":0}
引用次数: 0
Abstract
Motivated by the difficulty of accurately determining the inflow parameters in icing wind tunnels and flight tests, the Markov Chain Monte Carlo (MCMC) method, a commonly used Bayesian inference method, is explored to solve the inverse problem with the help of an icing software. The icing software, SJTUICE, is used to produce ice shapes for inversion and serves as the prediction tool in the iterations of the inversion problem. The influence of prior estimation of different icing parameters on the convergence and accuracy of the inversion problem is discussed. The feasibility of the MCMC method in inferring the inflow condition in terms of rime ice and glaze ice is assessed. Generally, fast convergence and good accuracy in terms of single inflow parameter inversion can be easily achieved. However, the number of iterations required increases rapidly with the number of inflow parameters in the MCMC method.
期刊介绍:
Aerospace Systems provides an international, peer-reviewed forum which focuses on system-level research and development regarding aeronautics and astronautics. The journal emphasizes the unique role and increasing importance of informatics on aerospace. It fills a gap in current publishing coverage from outer space vehicles to atmospheric vehicles by highlighting interdisciplinary science, technology and engineering.
Potential topics include, but are not limited to:
Trans-space vehicle systems design and integration
Air vehicle systems
Space vehicle systems
Near-space vehicle systems
Aerospace robotics and unmanned system
Communication, navigation and surveillance
Aerodynamics and aircraft design
Dynamics and control
Aerospace propulsion
Avionics system
Opto-electronic system
Air traffic management
Earth observation
Deep space exploration
Bionic micro-aircraft/spacecraft
Intelligent sensing and Information fusion