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Applied aerodynamics : papers presented at the AIAA SciTech Forum and Exposition 2020 : Orlando, Florida, USA, 6-10 January 2020. AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.)最新文献

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Correction: A Preliminary Investigation of the Secondary Flame and Operational Properties of an Actively-valved Pulse Jet 修正:主动阀脉冲射流的二次火焰和工作特性的初步研究
Xuren Zhu, Joel C. Lisanti, T. Guiberti, W. Roberts
Due to their complex nature, a clear and comprehensive understanding of the mechanisms driving the combustion dynamics of pulse jets is not yet available. The present work intends to fill this gap by shedding some light on general operational properties of an active valve resonant pulse combustor as well as fundamental mechanisms. Pressure sensors and ion probes were used to quantify the global performance of the pulse combustor in naturallyaspirated mode or for different forced air flow-rates. It was shown that performance, here indicated by the pressure gain, improves when the forced air flow-rate increases. For a subset of operating conditions, infrared and thermocouple thermometry was used to measure side wall temperatures. Gas sampling was also used to infer species concentrations inside the combustor and along its main axis. These measurements highlighted the presence of a secondary flame located in the tail pipe, near the exhaust. A possible mechanism responsible for this secondary flame was proposed.
由于脉冲射流的复杂性质,对其燃烧动力学的驱动机制还没有一个清晰而全面的认识。本工作旨在通过揭示主动阀谐振脉冲燃烧器的一般工作特性以及基本机理来填补这一空白。使用压力传感器和离子探针来量化脉冲燃烧器在自然吸气模式或不同强制空气流量下的整体性能。结果表明,当强迫空气流量增加时,性能(这里用压力增益表示)得到改善。对于一个子集的操作条件,红外和热电偶测温被用来测量侧壁温度。气体取样也被用来推断燃烧器内及其主轴的物质浓度。这些测量结果突出了位于尾管中靠近排气口的二次火焰的存在。提出了产生二次火焰的可能机理。
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引用次数: 0
CFD Concepts for In-Tunnel Simulation of Low Speed Wind Tunnels with Closed Test Section 封闭试验段低速风洞洞内模拟的CFD概念
R. Rudnik, S. Melber-Wilkending
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引用次数: 1
Effect of CO2and N2Dilution on Forced Ignition of Jet A/air Mixtures co2和n2稀释对喷射A/空气混合物强制点火的影响
Kaz Teope, Jonathan M. Bonebrake, D. Blunck
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引用次数: 0
Correction: Comparison of RADAR, Passive Optical with Acoustic, and Fused Multi-Modal Active and Passive Sensing for UAS Traffic Management Compliance and Urban Air Mobility Safety 修正:雷达、被动光学与声学、融合多模态主动与被动传感对无人机交通管理合规性和城市空中交通安全的比较
Sam Siewert, M. Andalibi, S. Bruder, Jonathan M. Buchholz, Doug Chamberlain, Alexandra L. Lindsey, Trevis Shiroma, David Stockhouse
Embry Riddle Aeronautical University Prescott has designed and prototyped a small UAS (Unmanned Aerial System) detection, tracking, classification and identification system for UTM (UAS Traffic Management) compliance verification and UAM (Urban Air Mobility). This system primarily uses passive optical and acoustic sensors along with GNSS (Global Navigation Satellite Systems), or GPS (Global Positioning System) and ADS-B (Automatic Dependent Surveillance Broadcast). The system design, known as Drone Net, is a network of passive sensors designed to cover a kilometer square area. In this paper we present the results of experiments to add an active RADAR (Radio Detection and Ranging) on the ground and active LIDAR (Light Detection and Ranging) on flight nodes (small UAS). System tests completed previously have shown feasibility for all passive optical and acoustic UTM and UAM. The point of the RADAR testing is to directly compare passive sensor networks to active to determine the value of each alone and to test the hypothesis that multimodal active and passive sensing will be superior, but likely at higher cost than passive alone. Previously, we completed coordinated experiments with an EO/IR camera system and acoustic sensor network with an Allsky hemispherical six-camera system with resolution up to 12 million pixels to optimize detection and tracking. For some applications such as corporate campuses and Class-D airports, passive sensing alone might be sufficient and most cost effective, but for urban, military, and higher traffic Class-C and Class-B larger airports, we believe the combined multi-modal purpose-built sUAS RADAR integrated with optical and acoustic sensor networks will be most effective. Based upon our preliminary results presented herein, purpose built small RADAR with wide fields of view configured into an All-sky active system along with optical All-sky cameras and acoustic sensors are ideal for urban locations requiring the highest confidence in monitoring of combined UTM, UAM and GA (General Aviation) traffic. UTM will mostly be small UAS delivering parcels and must share airspace with UAM carrying passengers for short-hop transportation along with general aviation covering longer distances, but also entering urban airspace at airports. Clearly the airspace in urban locations is going to become much more congested, with new risk, but also new opportunity to improve transportation overall. The results we present here are a start at answering basic questions about multi-modal sensor effectiveness for urban navigation, both passive and active. In scenarios where sUAS and UAM may not have reliable GNSS or might not be UTM compliant, the ground detection, tracking and localization is most critical for assured urban airspace safety and security.
Embry Riddle航空大学Prescott设计了一个小型UAS(无人机系统)检测、跟踪、分类和识别系统的原型,用于UTM(无人机交通管理)合规性验证和UAM(城市空中机动)。该系统主要使用无源光学和声学传感器以及GNSS(全球导航卫星系统)或GPS(全球定位系统)和ADS-B(自动相关监视广播)。该系统设计被称为无人机网络,是一个被动传感器网络,旨在覆盖一平方公里的区域。在本文中,我们介绍了在地面上添加有源雷达(无线电探测和测距)和在飞行节点(小型无人机)上添加有源激光雷达(光探测和测距)的实验结果。之前完成的系统测试显示了所有无源光学和声学UTM和UAM的可行性。RADAR测试的重点是直接比较被动传感器网络和主动传感器网络,以确定每个传感器网络单独的价值,并验证多模态主动和被动传感器网络更优越的假设,但可能比被动传感器网络的成本更高。之前,我们完成了EO/IR相机系统和声学传感器网络的协调实验,Allsky半球六摄像头系统的分辨率高达1200万像素,以优化检测和跟踪。对于一些应用,如企业园区和d类机场,单靠被动传感可能就足够了,而且最具成本效益,但对于城市、军事和更高流量的c类和b类大型机场,我们认为将多模态专用sUAS雷达与光学和声学传感器网络集成在一起将是最有效的。根据我们在本文中提出的初步结果,专用小型雷达具有宽视场,配置为全天主动系统,以及光学全天相机和声学传感器,非常适合城市位置,需要最高的信心来监测UTM, UAM和GA(通用航空)交通。UTM将主要是运送包裹的小型无人机,必须与载有乘客的UAM共享空域,进行短途运输,以及覆盖较长距离的通用航空,但也要进入机场的城市空域。显然,城市地区的空域将变得更加拥挤,这带来了新的风险,但也带来了改善整体交通的新机遇。我们在这里提出的结果是回答关于城市导航多模态传感器有效性的基本问题的开始,包括被动和主动。在sUAS和UAM可能没有可靠的GNSS或可能不符合UTM的情况下,地面探测、跟踪和定位对于确保城市空域安全和保障至关重要。
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引用次数: 1
Molecular recombination pathways of oxygen from quasiclassical trajectory calculations of the O3system 从o3体系准经典轨迹计算氧的分子重组路径
Chaithanya Kondur, K. Stephani
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引用次数: 1
Lagrangian Coherent Structures in Optimal Vortex Ring Formation 最佳涡环形成中的拉格朗日相干结构
B. Harter, J. Gregory
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引用次数: 0
Correction: Drag Coefficients of Circular Cylinders with Fineness Ratios of less than 0.50 measured by 0.1 and 0.3 m Magnetic Suspension and Balance Systems 修正:0.1米和0.3米磁悬浮和平衡系统测量细度比小于0.50的圆柱体阻力系数
Masahide Kuwata, Sho Yokota, H. Sawada, Yoshiaki Abe, A. Yakeno, T. Nonomura, K. Asai, S. Obayashi
{"title":"Correction: Drag Coefficients of Circular Cylinders with Fineness Ratios of less than 0.50 measured by 0.1 and 0.3 m Magnetic Suspension and Balance Systems","authors":"Masahide Kuwata, Sho Yokota, H. Sawada, Yoshiaki Abe, A. Yakeno, T. Nonomura, K. Asai, S. Obayashi","doi":"10.2514/6.2020-1325.c1","DOIUrl":"https://doi.org/10.2514/6.2020-1325.c1","url":null,"abstract":"","PeriodicalId":93413,"journal":{"name":"Applied aerodynamics : papers presented at the AIAA SciTech Forum and Exposition 2020 : Orlando, Florida, USA, 6-10 January 2020. AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.)","volume":"2 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2020-01-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"89336037","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
Surface pressure and coherent structure evolution on an axially accelerated delta wing 轴向加速三角翼表面压力与相干结构演化
Han Tu, M. Marzanek, Melissa A. Green, D. Rival
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引用次数: 0
Applications of Polynomial Chaos-Based Cokriging to Aerodynamic Design Optimization Benchmark Problems 基于多项式混沌的Cokriging在气动设计优化基准问题中的应用
J. Nagawkar, Leifur Þ. Leifsson, Xiaosong Du
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引用次数: 6
Correction: Numerical Study of Shock Interference Patterns for Gas Flows with Thermal Nonequilibrium and Finite-Rate Chemistry 修正:热非平衡和有限速率化学气体流动激波干涉模式的数值研究
C. Garbacz, M. Fossati, W. Maier, J. Alonso, J. Scoggins, T. Magin, T. Economon
{"title":"Correction: Numerical Study of Shock Interference Patterns for Gas Flows with Thermal Nonequilibrium and Finite-Rate Chemistry","authors":"C. Garbacz, M. Fossati, W. Maier, J. Alonso, J. Scoggins, T. Magin, T. Economon","doi":"10.2514/6.2020-1805.c1","DOIUrl":"https://doi.org/10.2514/6.2020-1805.c1","url":null,"abstract":"","PeriodicalId":93413,"journal":{"name":"Applied aerodynamics : papers presented at the AIAA SciTech Forum and Exposition 2020 : Orlando, Florida, USA, 6-10 January 2020. AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.)","volume":"76 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2020-01-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"79041661","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
期刊
Applied aerodynamics : papers presented at the AIAA SciTech Forum and Exposition 2020 : Orlando, Florida, USA, 6-10 January 2020. AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.)
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