J. Galindo, R. Navarro, L. García-Cuevas, B. Pallás
{"title":"超级高铁车辆瞬态任务经济高效CFD建模技术的发展","authors":"J. Galindo, R. Navarro, L. García-Cuevas, B. Pallás","doi":"10.1016/j.jweia.2025.106153","DOIUrl":null,"url":null,"abstract":"<div><div>Hyperloop system represents a promising alternative to the conventional means of transportation to face the critical environmental situation. Unfortunately, CFD modeling of hyperloop transient missions with a standard overset approach presents a high computational effort. This work aims to develop a methodology that reduces the cost of modeling a simplified pod with a three-phase operation: acceleration, cruise and deceleration. Firstly, a comparison between an overset domain and one employing Non-Reflecting Boundary Conditions (NRBCs) is conducted, resulting in a halving of the computational time and obtaining deviations of just 2.4% in vehicle drag. However, the larger reduction in cost comes with the development of an equivalent quasi-steady state configuration for hyperloop systems. The leading contribution of this paper is that the proposed approach considers the effect of the induced mass flow generated by the effect of moving a pod inside a tube, a non-negligible effect. Such a novel method helps reduce the error in terms of drag coefficient, which can achieve values higher than 40% if the boundary conditions for the steady state are not properly corrected. Consequently, the proposed method reduces simulations cost up to 35 times with an average error of only the 4% in power requirement predictions.</div></div>","PeriodicalId":54752,"journal":{"name":"Journal of Wind Engineering and Industrial Aerodynamics","volume":"264 ","pages":"Article 106153"},"PeriodicalIF":4.2000,"publicationDate":"2025-06-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Development of cost-effective CFD modeling techniques for transient missions of hyperloop vehicles\",\"authors\":\"J. Galindo, R. Navarro, L. García-Cuevas, B. Pallás\",\"doi\":\"10.1016/j.jweia.2025.106153\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Hyperloop system represents a promising alternative to the conventional means of transportation to face the critical environmental situation. Unfortunately, CFD modeling of hyperloop transient missions with a standard overset approach presents a high computational effort. This work aims to develop a methodology that reduces the cost of modeling a simplified pod with a three-phase operation: acceleration, cruise and deceleration. Firstly, a comparison between an overset domain and one employing Non-Reflecting Boundary Conditions (NRBCs) is conducted, resulting in a halving of the computational time and obtaining deviations of just 2.4% in vehicle drag. However, the larger reduction in cost comes with the development of an equivalent quasi-steady state configuration for hyperloop systems. The leading contribution of this paper is that the proposed approach considers the effect of the induced mass flow generated by the effect of moving a pod inside a tube, a non-negligible effect. Such a novel method helps reduce the error in terms of drag coefficient, which can achieve values higher than 40% if the boundary conditions for the steady state are not properly corrected. Consequently, the proposed method reduces simulations cost up to 35 times with an average error of only the 4% in power requirement predictions.</div></div>\",\"PeriodicalId\":54752,\"journal\":{\"name\":\"Journal of Wind Engineering and Industrial Aerodynamics\",\"volume\":\"264 \",\"pages\":\"Article 106153\"},\"PeriodicalIF\":4.2000,\"publicationDate\":\"2025-06-30\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Journal of Wind Engineering and Industrial Aerodynamics\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0167610525001497\",\"RegionNum\":2,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, CIVIL\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Journal of Wind Engineering and Industrial Aerodynamics","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0167610525001497","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, CIVIL","Score":null,"Total":0}
Development of cost-effective CFD modeling techniques for transient missions of hyperloop vehicles
Hyperloop system represents a promising alternative to the conventional means of transportation to face the critical environmental situation. Unfortunately, CFD modeling of hyperloop transient missions with a standard overset approach presents a high computational effort. This work aims to develop a methodology that reduces the cost of modeling a simplified pod with a three-phase operation: acceleration, cruise and deceleration. Firstly, a comparison between an overset domain and one employing Non-Reflecting Boundary Conditions (NRBCs) is conducted, resulting in a halving of the computational time and obtaining deviations of just 2.4% in vehicle drag. However, the larger reduction in cost comes with the development of an equivalent quasi-steady state configuration for hyperloop systems. The leading contribution of this paper is that the proposed approach considers the effect of the induced mass flow generated by the effect of moving a pod inside a tube, a non-negligible effect. Such a novel method helps reduce the error in terms of drag coefficient, which can achieve values higher than 40% if the boundary conditions for the steady state are not properly corrected. Consequently, the proposed method reduces simulations cost up to 35 times with an average error of only the 4% in power requirement predictions.
期刊介绍:
The objective of the journal is to provide a means for the publication and interchange of information, on an international basis, on all those aspects of wind engineering that are included in the activities of the International Association for Wind Engineering http://www.iawe.org/. These are: social and economic impact of wind effects; wind characteristics and structure, local wind environments, wind loads and structural response, diffusion, pollutant dispersion and matter transport, wind effects on building heat loss and ventilation, wind effects on transport systems, aerodynamic aspects of wind energy generation, and codification of wind effects.
Papers on these subjects describing full-scale measurements, wind-tunnel simulation studies, computational or theoretical methods are published, as well as papers dealing with the development of techniques and apparatus for wind engineering experiments.