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Wind Tunnel Testing of Tethered Inflatable Wings 系留充气式机翼的风洞试验
IF 2.2 3区 工程技术
Journal of Aircraft Pub Date : 2024-07-23 DOI: 10.2514/1.c037437
Siddhant Desai, Joseph A. Schetz, Rakesh K. Kapania, Rikin Gupta
{"title":"Wind Tunnel Testing of Tethered Inflatable Wings","authors":"Siddhant Desai, Joseph A. Schetz, Rakesh K. Kapania, Rikin Gupta","doi":"10.2514/1.c037437","DOIUrl":"https://doi.org/10.2514/1.c037437","url":null,"abstract":"Journal of Aircraft, Ahead of Print. <br/>","PeriodicalId":14927,"journal":{"name":"Journal of Aircraft","volume":null,"pages":null},"PeriodicalIF":2.2,"publicationDate":"2024-07-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141778427","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
High-Lift Aerodynamics of Integrated Distributed Propulsion Systems with Thrust Vectoring 带推力矢量的集成分布式推进系统的高扬程空气动力学
IF 2.2 3区 工程技术
Journal of Aircraft Pub Date : 2024-07-09 DOI: 10.2514/1.c037902
Himavath Jois, Alan S. Hong, Phillip J. Ansell
{"title":"High-Lift Aerodynamics of Integrated Distributed Propulsion Systems with Thrust Vectoring","authors":"Himavath Jois, Alan S. Hong, Phillip J. Ansell","doi":"10.2514/1.c037902","DOIUrl":"https://doi.org/10.2514/1.c037902","url":null,"abstract":"Journal of Aircraft, Ahead of Print. <br/>","PeriodicalId":14927,"journal":{"name":"Journal of Aircraft","volume":null,"pages":null},"PeriodicalIF":2.2,"publicationDate":"2024-07-09","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141573463","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Power Setting Estimation of Departing Civil Jet Aircraft Based on Machine Learning 基于机器学习的离港民用喷气式飞机功率设置估计
IF 2.2 3区 工程技术
Journal of Aircraft Pub Date : 2024-07-09 DOI: 10.2514/1.c037619
Jonas Meister
{"title":"Power Setting Estimation of Departing Civil Jet Aircraft Based on Machine Learning","authors":"Jonas Meister","doi":"10.2514/1.c037619","DOIUrl":"https://doi.org/10.2514/1.c037619","url":null,"abstract":"Journal of Aircraft, Ahead of Print. <br/>","PeriodicalId":14927,"journal":{"name":"Journal of Aircraft","volume":null,"pages":null},"PeriodicalIF":2.2,"publicationDate":"2024-07-09","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141573465","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Steady Versus Unsteady Pneumatic Flow Control and Aspects of Practical Integration 稳态与非稳态气动流量控制以及实际集成的各个方面
IF 2.2 3区 工程技术
Journal of Aircraft Pub Date : 2024-06-27 DOI: 10.2514/1.c037673
Arvin Shmilovich, Abdi Khodadoust, Christopher R. Colletti, Phillip J. Ansell
{"title":"Steady Versus Unsteady Pneumatic Flow Control and Aspects of Practical Integration","authors":"Arvin Shmilovich, Abdi Khodadoust, Christopher R. Colletti, Phillip J. Ansell","doi":"10.2514/1.c037673","DOIUrl":"https://doi.org/10.2514/1.c037673","url":null,"abstract":"Journal of Aircraft, Ahead of Print. <br/>","PeriodicalId":14927,"journal":{"name":"Journal of Aircraft","volume":null,"pages":null},"PeriodicalIF":2.2,"publicationDate":"2024-06-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141521267","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Thermomechanical Collaborative Design and Experimental Verification of a Sandwich Structure with a Polyimide Foam Core 带聚酰亚胺泡沫芯材的三明治结构的热力学协同设计与实验验证
IF 2.2 3区 工程技术
Journal of Aircraft Pub Date : 2024-06-27 DOI: 10.2514/1.c037780
Zhang Long, Luo Wenbo, Zhao Xin, Zhao Yunpeng
{"title":"Thermomechanical Collaborative Design and Experimental Verification of a Sandwich Structure with a Polyimide Foam Core","authors":"Zhang Long, Luo Wenbo, Zhao Xin, Zhao Yunpeng","doi":"10.2514/1.c037780","DOIUrl":"https://doi.org/10.2514/1.c037780","url":null,"abstract":"Journal of Aircraft, Ahead of Print. <br/>","PeriodicalId":14927,"journal":{"name":"Journal of Aircraft","volume":null,"pages":null},"PeriodicalIF":2.2,"publicationDate":"2024-06-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141500729","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Experimental and Numerical Investigations of Mini-Tab Device for Active Flow Control 用于主动流量控制的微型平板装置的实验和数值研究
IF 2.2 3区 工程技术
Journal of Aircraft Pub Date : 2024-06-27 DOI: 10.2514/1.c037766
Sam Bull, Dami Adeyemi, Dom Wilson, David Cleaver, Jon du Bois
{"title":"Experimental and Numerical Investigations of Mini-Tab Device for Active Flow Control","authors":"Sam Bull, Dami Adeyemi, Dom Wilson, David Cleaver, Jon du Bois","doi":"10.2514/1.c037766","DOIUrl":"https://doi.org/10.2514/1.c037766","url":null,"abstract":"Journal of Aircraft, Ahead of Print. <br/>","PeriodicalId":14927,"journal":{"name":"Journal of Aircraft","volume":null,"pages":null},"PeriodicalIF":2.2,"publicationDate":"2024-06-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141521266","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Ice Shape Convergence in Multistep Ice Accretion Simulations 多步冰堆积模拟中的冰形趋同
IF 2.2 3区 工程技术
Journal of Aircraft Pub Date : 2024-06-27 DOI: 10.2514/1.c037887
Alessandro Donizetti, Tommaso Bellosta, Alberto Guardone
{"title":"Ice Shape Convergence in Multistep Ice Accretion Simulations","authors":"Alessandro Donizetti, Tommaso Bellosta, Alberto Guardone","doi":"10.2514/1.c037887","DOIUrl":"https://doi.org/10.2514/1.c037887","url":null,"abstract":"Journal of Aircraft, Ahead of Print. <br/>","PeriodicalId":14927,"journal":{"name":"Journal of Aircraft","volume":null,"pages":null},"PeriodicalIF":2.2,"publicationDate":"2024-06-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141500733","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Effect of Adhesive Layer Thickness on Strength of Carbon-Fiber-Reinforced Plastic/Aluminum Bond-Riveted Joints 粘合剂层厚度对碳纤维增强塑料/铝粘合铆接强度的影响
IF 2.2 3区 工程技术
Journal of Aircraft Pub Date : 2024-06-25 DOI: 10.2514/1.c037752
Chengxiang Guo, Minghao Zhang, Lubin Huo, Zengqaing Cao
{"title":"Effect of Adhesive Layer Thickness on Strength of Carbon-Fiber-Reinforced Plastic/Aluminum Bond-Riveted Joints","authors":"Chengxiang Guo, Minghao Zhang, Lubin Huo, Zengqaing Cao","doi":"10.2514/1.c037752","DOIUrl":"https://doi.org/10.2514/1.c037752","url":null,"abstract":"Journal of Aircraft, Ahead of Print. <br/>","PeriodicalId":14927,"journal":{"name":"Journal of Aircraft","volume":null,"pages":null},"PeriodicalIF":2.2,"publicationDate":"2024-06-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141500730","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Control Authority of a Single-Surface Parafoil with Bleed-Air Spoilers 带有放气扰流板的单面伞翼的控制权
IF 2.2 3区 工程技术
Journal of Aircraft Pub Date : 2024-06-10 DOI: 10.2514/1.c037791
Donald J. Ward, Andrea L. Vu, Mark Costello
{"title":"Control Authority of a Single-Surface Parafoil with Bleed-Air Spoilers","authors":"Donald J. Ward, Andrea L. Vu, Mark Costello","doi":"10.2514/1.c037791","DOIUrl":"https://doi.org/10.2514/1.c037791","url":null,"abstract":"Bleed-air control of ram-air parafoils is a lightweight and cost-effective mechanism that enables significant landing accuracy improvements compared to traditional trailing edge brake control due to the addition of direct glide slope control. Single-surface parafoil canopies have been shown to be lightweight and possess similar flight behavior as their ram-air counterparts. The design of bleed-air spoilers is more challenging for single-surface canopies, which lack the internal ram-air that provides a high pressure differential at any chordwise location. This paper explores bleed-air spoilers on single-surface parafoils with a focus on turn rate and glide slope control capabilities. Through a flight test campaign, it was shown that bleed-air spoilers on a single-surface parafoil provide both turn rate control from asymmetric vent opening and glide slope change from symmetric vent opening. Vents located far forward at the 10% chord location yield substantial control response with a maximum turn rate response of 38 deg/s and a maximum glide slope change of 58%. Vents located farther aft at 30, 50, and 70% chords demonstrated diminished control authority. Varying the spanwise locations of the spoilers revealed that the outermost vents had negligible lateral and longitudinal control authority.","PeriodicalId":14927,"journal":{"name":"Journal of Aircraft","volume":null,"pages":null},"PeriodicalIF":2.2,"publicationDate":"2024-06-10","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141362426","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Research on Anti-Rollover Adaptive Landing Gear Technology Based on Impedance Control 基于阻抗控制的防侧翻自适应起落架技术研究
IF 2.2 3区 工程技术
Journal of Aircraft Pub Date : 2024-06-10 DOI: 10.2514/1.c037491
Hao Qi, Zi-Chao Chen, Yi-Ming Peng, Hong Nie, Xiao-Hui Wei, Qing-Yang Li
{"title":"Research on Anti-Rollover Adaptive Landing Gear Technology Based on Impedance Control","authors":"Hao Qi, Zi-Chao Chen, Yi-Ming Peng, Hong Nie, Xiao-Hui Wei, Qing-Yang Li","doi":"10.2514/1.c037491","DOIUrl":"https://doi.org/10.2514/1.c037491","url":null,"abstract":"During the Vertical Take-Off and Landing (VTOL) of a rotorcraft, there is a high risk of instability and safety incidents due to the possibility of one side of the landing gear making initial contact with the ground, particularly under extreme environmental conditions and maneuvers. Furthermore, the varied performance of adaptive landing gear necessitates a landing control approach that specifically targets both sides of the adaptive landing gear. This study proposes a method that regulates the landing gear first touchdown side through an impedance controller to guarantee the stability of the rotorcraft and then tilts the landing gear toward the rear landing leg side, followed by a soft and smooth landing through the rear landing leg. This approach accomplishes steady adaptive VTOL of the rotorcraft. The fall vibration test results demonstrate that the adaptive landing gear system with impedance control has excellent adaptive landing functionality, which can handle not only landing on uneven ground at various points but also cope with different ascent rates and ground friction during stable takeoff/landing.","PeriodicalId":14927,"journal":{"name":"Journal of Aircraft","volume":null,"pages":null},"PeriodicalIF":2.2,"publicationDate":"2024-06-10","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141364090","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":3,"RegionCategory":"工程技术","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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