CEAS Aeronautical Journal最新文献

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Experimental and numerical analysis of the aerodynamics and vortex interactions on multi-swept delta wings 多掠三角翼气动与涡相互作用的实验与数值分析
CEAS Aeronautical Journal Pub Date : 2023-08-26 DOI: 10.1007/s13272-023-00678-7
M. Werner, M. Rein, K. Richter, S. Weiss
{"title":"Experimental and numerical analysis of the aerodynamics and vortex interactions on multi-swept delta wings","authors":"M. Werner, M. Rein, K. Richter, S. Weiss","doi":"10.1007/s13272-023-00678-7","DOIUrl":"https://doi.org/10.1007/s13272-023-00678-7","url":null,"abstract":"Abstract The flow field around a generic multi-swept delta wing configuration is investigated under transonic flow conditions, both experimentally and numerically. A special focus is on the analysis of vortex/vortex and vortex/shock interactions at moderate angles of attack. In the present study, the Mach number is varied between $$textrm{Ma} = {0.50}$$ <mml:math xmlns:mml=\"http://www.w3.org/1998/Math/MathML\"> <mml:mrow> <mml:mtext>Ma</mml:mtext> <mml:mo>=</mml:mo> <mml:mrow> <mml:mn>0.50</mml:mn> </mml:mrow> </mml:mrow> </mml:math> and $$textrm{Ma} = {1.41}$$ <mml:math xmlns:mml=\"http://www.w3.org/1998/Math/MathML\"> <mml:mrow> <mml:mtext>Ma</mml:mtext> <mml:mo>=</mml:mo> <mml:mrow> <mml:mn>1.41</mml:mn> </mml:mrow> </mml:mrow> </mml:math> and the angle of attack is varied between $$alpha = 8^circ$$ <mml:math xmlns:mml=\"http://www.w3.org/1998/Math/MathML\"> <mml:mrow> <mml:mi>α</mml:mi> <mml:mo>=</mml:mo> <mml:msup> <mml:mn>8</mml:mn> <mml:mo>∘</mml:mo> </mml:msup> </mml:mrow> </mml:math> and $$alpha = 28^circ$$ <mml:math xmlns:mml=\"http://www.w3.org/1998/Math/MathML\"> <mml:mrow> <mml:mi>α</mml:mi> <mml:mo>=</mml:mo> <mml:msup> <mml:mn>28</mml:mn> <mml:mo>∘</mml:mo> </mml:msup> </mml:mrow> </mml:math> . Numerical results are validated using experimental surface pressure data from pressure taps, as well as forces and moments based on strain gauge measurements. For selected cases, velocity field data from particle image velocimetry (PIV) measurements are available as well. Over a broad range of angle of attack and Mach number, strong vortex/vortex interactions, including vortex braiding and vortex merging, occur. The location of vortex merging is moving downstream with increasing angle of attack and increasing Mach number. Additionally, at $$textrm{Ma} = {0.85}$$ <mml:math xmlns:mml=\"http://www.w3.org/1998/Math/MathML\"> <mml:mrow> <mml:mtext>Ma</mml:mtext> <mml:mo>=</mml:mo> <mml:mrow> <mml:mn>0.85</mml:mn> </mml:mrow> </mml:mrow> </mml:math> , vortex/shock interaction occurs above the wing. For moderate angles of attack, shock-induced vortex breakdown is observed.","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":"133 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2023-08-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"135181507","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
High-resolution vibroacoustic characterization of DLR’s Falcon 2000LX ISTAR aircraft 德国航空航天中心Falcon 2000LX ISTAR飞机的高分辨率振动声特性
CEAS Aeronautical Journal Pub Date : 2023-08-24 DOI: 10.1007/s13272-023-00676-9
R. Winter, M. Norambuena, J. Sinske, Sebastian Zettel
{"title":"High-resolution vibroacoustic characterization of DLR’s Falcon 2000LX ISTAR aircraft","authors":"R. Winter, M. Norambuena, J. Sinske, Sebastian Zettel","doi":"10.1007/s13272-023-00676-9","DOIUrl":"https://doi.org/10.1007/s13272-023-00676-9","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":"1 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2023-08-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"41901162","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 multi-model and multi-objective approach to the design of helicopter flight control laws 直升机飞行控制律设计的多模型多目标方法
CEAS Aeronautical Journal Pub Date : 2023-07-06 DOI: 10.1007/s13272-023-00675-w
Patrick Authié
{"title":"A multi-model and multi-objective approach to the design of helicopter flight control laws","authors":"Patrick Authié","doi":"10.1007/s13272-023-00675-w","DOIUrl":"https://doi.org/10.1007/s13272-023-00675-w","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":" ","pages":""},"PeriodicalIF":0.0,"publicationDate":"2023-07-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"47799836","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
Nonlinear system identification of a UAV model with distributed aerodynamics and flexible structure 具有分布式空气动力学和柔性结构的无人机模型的非线性系统辨识
CEAS Aeronautical Journal Pub Date : 2023-07-01 DOI: 10.1007/s13272-023-00674-x
Benjamín Herrmann, J. Theis, F. Thielecke
{"title":"Nonlinear system identification of a UAV model with distributed aerodynamics and flexible structure","authors":"Benjamín Herrmann, J. Theis, F. Thielecke","doi":"10.1007/s13272-023-00674-x","DOIUrl":"https://doi.org/10.1007/s13272-023-00674-x","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":"14 1","pages":"661 - 677"},"PeriodicalIF":0.0,"publicationDate":"2023-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"47578406","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
Robust gain-scheduled autopilot design with anti-windup compensation for a guided projectile 制导炮弹具有抗饱和补偿的鲁棒增益调度自动驾驶仪设计
CEAS Aeronautical Journal Pub Date : 2023-07-01 DOI: 10.1007/s13272-023-00668-9
Sovanna Thai, S. Theodoulis, C. Roos, J. Biannic
{"title":"Robust gain-scheduled autopilot design with anti-windup compensation for a guided projectile","authors":"Sovanna Thai, S. Theodoulis, C. Roos, J. Biannic","doi":"10.1007/s13272-023-00668-9","DOIUrl":"https://doi.org/10.1007/s13272-023-00668-9","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":"14 1","pages":"765 - 786"},"PeriodicalIF":0.0,"publicationDate":"2023-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"49316569","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
Effects of an enhanced fibre–matrix adhesion on the fatigue behaviour of composite materials under very high cycle fatigue 纤维基质黏附增强对复合材料高周疲劳性能的影响
CEAS Aeronautical Journal Pub Date : 2023-07-01 DOI: 10.1007/s13272-023-00673-y
M. Bartelt, P. Horst, S. Heimbs
{"title":"Effects of an enhanced fibre–matrix adhesion on the fatigue behaviour of composite materials under very high cycle fatigue","authors":"M. Bartelt, P. Horst, S. Heimbs","doi":"10.1007/s13272-023-00673-y","DOIUrl":"https://doi.org/10.1007/s13272-023-00673-y","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":"14 1","pages":"753 - 763"},"PeriodicalIF":0.0,"publicationDate":"2023-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"45948094","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
Numerical studies on small rotor configurations with validation using acoustic wind tunnel data 小转子结构的数值研究及声学风洞数据的验证
CEAS Aeronautical Journal Pub Date : 2023-06-30 DOI: 10.1007/s13272-023-00671-0
J. Yin, Karl-Stéphane Rossignol, Lukas Rottmann, T. Schwarz
{"title":"Numerical studies on small rotor configurations with validation using acoustic wind tunnel data","authors":"J. Yin, Karl-Stéphane Rossignol, Lukas Rottmann, T. Schwarz","doi":"10.1007/s13272-023-00671-0","DOIUrl":"https://doi.org/10.1007/s13272-023-00671-0","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":" ","pages":""},"PeriodicalIF":0.0,"publicationDate":"2023-06-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"47115513","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
Identifying challenges in maintenance planning for on-demand UAM fleets using agent-based simulations 使用基于代理的模拟,识别按需UAM车队维护计划中的挑战
CEAS Aeronautical Journal Pub Date : 2023-06-27 DOI: 10.1007/s13272-023-00665-y
Patrick Sieb, J. Michelmann, F. Flöter, K. Wicke
{"title":"Identifying challenges in maintenance planning for on-demand UAM fleets using agent-based simulations","authors":"Patrick Sieb, J. Michelmann, F. Flöter, K. Wicke","doi":"10.1007/s13272-023-00665-y","DOIUrl":"https://doi.org/10.1007/s13272-023-00665-y","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":"14 1","pages":"637 - 660"},"PeriodicalIF":0.0,"publicationDate":"2023-06-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"41395829","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: 2
Rotorcraft source noise characterization via acoustic snapshot array: development and evaluation 旋翼机声源噪声特性通过声快照阵列:发展和评估
CEAS Aeronautical Journal Pub Date : 2023-06-16 DOI: 10.1007/s13272-023-00672-z
James H. Stephenson, Mary L. Houston
{"title":"Rotorcraft source noise characterization via acoustic snapshot array: development and evaluation","authors":"James H. Stephenson, Mary L. Houston","doi":"10.1007/s13272-023-00672-z","DOIUrl":"https://doi.org/10.1007/s13272-023-00672-z","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":" ","pages":""},"PeriodicalIF":0.0,"publicationDate":"2023-06-16","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"44837964","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
Modelling of aircraft trajectories for emergency landing using kinematoid chains 用类运动学链建立飞机紧急降落轨迹模型
CEAS Aeronautical Journal Pub Date : 2023-06-16 DOI: 10.1007/s13272-023-00667-w
Steffen Flämig, Matthias Graefenhan, W. Schiffmann
{"title":"Modelling of aircraft trajectories for emergency landing using kinematoid chains","authors":"Steffen Flämig, Matthias Graefenhan, W. Schiffmann","doi":"10.1007/s13272-023-00667-w","DOIUrl":"https://doi.org/10.1007/s13272-023-00667-w","url":null,"abstract":"","PeriodicalId":38083,"journal":{"name":"CEAS Aeronautical Journal","volume":"14 1","pages":"679 - 692"},"PeriodicalIF":0.0,"publicationDate":"2023-06-16","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"44419741","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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