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CEAS Aeronautical Journal最新文献

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Exploration of optimal control based surrogate modeling as a basis for fuel efficient 4D aircraft routing on graphs 探索基于优化控制的代理建模,以此为基础在图上绘制燃油效率高的 4D 飞机航线
Q2 Engineering Pub Date : 2024-02-04 DOI: 10.1007/s13272-023-00710-w
Felix Schweighofer, B. Grüter, Florian Holzapfel
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引用次数: 1
Exploration of optimal control based surrogate modeling as a basis for fuel efficient 4D aircraft routing on graphs 探索基于优化控制的代理建模,以此为基础在图上绘制燃油效率高的 4D 飞机航线
Q2 Engineering Pub Date : 2024-02-04 DOI: 10.1007/s13272-023-00710-w
Felix Schweighofer, B. Grüter, Florian Holzapfel
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引用次数: 1
Correction to: Understanding the fixed pitch RPM-controlled rotor modeling for the conceptual design of UAM vehicles 更正:了解用于 UAM 飞行器概念设计的固定螺距转速控制转子模型
Q2 Engineering Pub Date : 2024-01-31 DOI: 10.1007/s13272-024-00713-1
K. Atci, P. Weiand, Feyyaz Guner
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引用次数: 0
Aerodynamic interactions between distributed propellers and the wing of an electric commuter aircraft at cruise conditions 巡航状态下电动通勤飞机的分布式螺旋桨与机翼之间的空气动力相互作用
Q2 Engineering Pub Date : 2024-01-18 DOI: 10.1007/s13272-023-00706-6
Michael Schollenberger, Bastian Kirsch, Thorsten Lutz, Ewald Krämer, Jens Friedrichs
{"title":"Aerodynamic interactions between distributed propellers and the wing of an electric commuter aircraft at cruise conditions","authors":"Michael Schollenberger, Bastian Kirsch, Thorsten Lutz, Ewald Krämer, Jens Friedrichs","doi":"10.1007/s13272-023-00706-6","DOIUrl":"https://doi.org/10.1007/s13272-023-00706-6","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":"111 40","pages":""},"PeriodicalIF":0.0,"publicationDate":"2024-01-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139614262","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Impact of 2D engine nacelle flow on buffet 二维发动机短舱气流对缓冲器的影响
Q2 Engineering Pub Date : 2024-01-01 DOI: 10.1007/s13272-024-00728-8
Thomas Lürkens, M. Meinke, Wolfgang Schröder
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引用次数: 0
Understanding the fixed pitch RPM-controlled rotor modeling for the conceptual design of UAM vehicles 了解用于 UAM 飞行器概念设计的固定螺距 RPM 控制转子模型
Q2 Engineering Pub Date : 2023-12-19 DOI: 10.1007/s13272-023-00703-9
Kagan Atci, P. Weiand, Feyyaz Guner
{"title":"Understanding the fixed pitch RPM-controlled rotor modeling for the conceptual design of UAM vehicles","authors":"Kagan Atci, P. Weiand, Feyyaz Guner","doi":"10.1007/s13272-023-00703-9","DOIUrl":"https://doi.org/10.1007/s13272-023-00703-9","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":" 11","pages":""},"PeriodicalIF":0.0,"publicationDate":"2023-12-19","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"138960131","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 1
Free fall drag estimation of small-scale multirotor unmanned aircraft systems using computational fluid dynamics and wind tunnel experiments 利用计算流体动力学和风洞试验估算小型多旋翼无人机系统的自由落体阻力
Q2 Engineering Pub Date : 2023-12-12 DOI: 10.1007/s13272-023-00702-w
T. Hammer, J. Quitter, J. Mayntz, J.-M. Bauschat, P. Dahmann, F. Götten, S. Hille, E. Stumpf
{"title":"Free fall drag estimation of small-scale multirotor unmanned aircraft systems using computational fluid dynamics and wind tunnel experiments","authors":"T. Hammer, J. Quitter, J. Mayntz, J.-M. Bauschat, P. Dahmann, F. Götten, S. Hille, E. Stumpf","doi":"10.1007/s13272-023-00702-w","DOIUrl":"https://doi.org/10.1007/s13272-023-00702-w","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":"16 23","pages":""},"PeriodicalIF":0.0,"publicationDate":"2023-12-12","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139009504","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
A method for an efficiency and weight-optimised preliminary design of a hydrogen-powered fuel cell-based hybrid-electric propulsion system for aviation purposes 航空氢燃料电池混合电力推进系统的效率和重量优化初步设计方法
Q2 Engineering Pub Date : 2023-12-10 DOI: 10.1007/s13272-023-00699-2
Mücahit Akkaya, Nicolai Neumann, Dieter Peitsch
{"title":"A method for an efficiency and weight-optimised preliminary design of a hydrogen-powered fuel cell-based hybrid-electric propulsion system for aviation purposes","authors":"Mücahit Akkaya, Nicolai Neumann, Dieter Peitsch","doi":"10.1007/s13272-023-00699-2","DOIUrl":"https://doi.org/10.1007/s13272-023-00699-2","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":"19 3‐4","pages":""},"PeriodicalIF":0.0,"publicationDate":"2023-12-10","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"138982145","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Evaluation of an automatic continuous high-lift system in a flight simulator study with airline pilots 以航空公司飞行员为对象的飞行模拟器研究中对自动连续高升力系统的评估
Q2 Engineering Pub Date : 2023-12-08 DOI: 10.1007/s13272-023-00700-y
Pia Eichhorn, Flávio Silvestre
{"title":"Evaluation of an automatic continuous high-lift system in a flight simulator study with airline pilots","authors":"Pia Eichhorn, Flávio Silvestre","doi":"10.1007/s13272-023-00700-y","DOIUrl":"https://doi.org/10.1007/s13272-023-00700-y","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":"44 37","pages":""},"PeriodicalIF":0.0,"publicationDate":"2023-12-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"138588523","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Comparison of shock-buffet dynamics on a supercritical airfoil with and without a pitching degree of freedom 有俯仰自由度和无俯仰自由度超临界机翼冲击缓冲动力学比较
Q2 Engineering Pub Date : 2023-11-24 DOI: 10.1007/s13272-023-00692-9
S. Scharnowski, Alessandro Accorinti, Tim Korthäuer, Christian J. Kähler
{"title":"Comparison of shock-buffet dynamics on a supercritical airfoil with and without a pitching degree of freedom","authors":"S. Scharnowski, Alessandro Accorinti, Tim Korthäuer, Christian J. Kähler","doi":"10.1007/s13272-023-00692-9","DOIUrl":"https://doi.org/10.1007/s13272-023-00692-9","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":"27 2","pages":""},"PeriodicalIF":0.0,"publicationDate":"2023-11-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139238804","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
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CEAS Aeronautical Journal
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