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Three-dimensional Shock Wave Interactions in Sabot Separation Launched in Hypersonic Regime 高超声速弹射分离中的三维激波相互作用
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.147
H. Kasahara, A. Matsuo
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引用次数: 0
Method of Suppressing Ingestion Particles Flowing Back to a Hall Thruster using a Beam Target during Ground Testing 地面试验中使用波束靶抑制吸入粒子流回霍尔推进器的方法
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.160
G. Ito, R. Kawashima, K. Komurasaki, H. Koizumi
{"title":"Method of Suppressing Ingestion Particles Flowing Back to a Hall Thruster using a Beam Target during Ground Testing","authors":"G. Ito, R. Kawashima, K. Komurasaki, H. Koizumi","doi":"10.2322/tjsass.65.160","DOIUrl":"https://doi.org/10.2322/tjsass.65.160","url":null,"abstract":"","PeriodicalId":54419,"journal":{"name":"Transactions of the Japan Society for Aeronautical and Space Sciences","volume":"1 1","pages":""},"PeriodicalIF":1.1,"publicationDate":"2022-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"68664458","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"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
Performance Evaluation of an Airborne Coherent Doppler Lidar and Investigation of Its Practical Application 机载相干多普勒激光雷达性能评价及实际应用研究
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.47
H. Inokuchi, T. Akiyama
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引用次数: 4
Modified Lifting Line Method Based on Vortex Rings and Its Application on Lift Fan Design 基于涡环的改进提升线法及其在提升风机设计中的应用
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.23
Haitong Wang, Yan’gang Wang, Si Wang, Fang Zhou, Hanru Liu
The image vortex model is widely used in lifting line method to predict the fl ow induced by the shroud and hub surface in ducted fan, but it does not perform well in lift fan design due to the zero far fi eld in fl ow. In this paper the theoretical defects and numerical error propagation characteristic of the image vortex model in simulating duct surface are studied. Then the vortex rings correction based on image vortex model is veri fi ed and applied in lifting line method. In order to test the improved method, a 150 mm diameter lift fan is designed by the modi fi ed lifting line method, after that, analyzed by the modi fi ed lifting line itself and RANS solver respectively. The results show that the contribution of the vortex rings at the rotor accounts for 50% of the total induced velocity, and it accounts for 35% at the stator, which veri fi es the necessity of the vortex rings correction. The performance of the rotor and stator geometry is consistent with the design expectation, the e ffi ciency is up to 90.97% by numerical simulation and 88.32% by experimental measurement, which con fi rms the reli-ability of the modi fi ed lifting line method developed in this paper especially on lift fan design.
升力线法中广泛采用像涡模型来预测导管式风机叶冠和轮毂表面诱导的气流,但由于气流中的远场为零,在升力风机设计中表现不佳。本文研究了像涡模型在模拟管道表面时的理论缺陷和数值误差传播特性。然后验证了基于图像涡模型的涡环校正方法,并将其应用于提升线法。为了验证改进后的方法,采用定矩提升线法设计了一个直径150mm的提升风机,然后分别用定矩提升线本身和RANS求解器进行了分析。结果表明,转子处涡流环的贡献占总感应速度的50%,定子处涡流环的贡献占总感应速度的35%,验证了涡流环校正的必要性。转子和定子几何形状的性能符合设计预期,数值模拟效率达90.97%,实验测量效率达88.32%,证实了本文提出的固定升力线方法特别是升力风机设计的可靠性。
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引用次数: 0
In-flight Profile Updates by Appropriate Cost Index Selection — Operational Perspective 通过适当的成本指数选择来更新飞行概况-操作角度
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.56
Ryota Mori
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引用次数: 1
Selecting Initial Gimbal Angles of Roof-type CMG System for Avoiding Singularities in Spacecraft Attitude Maneuver 为避免航天器姿态机动中的奇点,选择舱盖式CMG系统初始框架角
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.123
Haoxiang Liu, Satoshi Satoh, Y. Shoji, I. Jikuya, Katsuhiko Yamada
{"title":"Selecting Initial Gimbal Angles of Roof-type CMG System for Avoiding Singularities in Spacecraft Attitude Maneuver","authors":"Haoxiang Liu, Satoshi Satoh, Y. Shoji, I. Jikuya, Katsuhiko Yamada","doi":"10.2322/tjsass.65.123","DOIUrl":"https://doi.org/10.2322/tjsass.65.123","url":null,"abstract":"","PeriodicalId":54419,"journal":{"name":"Transactions of the Japan Society for Aeronautical and Space Sciences","volume":"1 1","pages":""},"PeriodicalIF":1.1,"publicationDate":"2022-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"68664239","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"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
Numerical Simulation of Jet Mixing in Supersonic Crossflow: Effect of Jet Exit Geometry 超声速横流中射流混合的数值模拟:射流出口几何形状的影响
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.172
T. Iwasa, N. Tsuboi
{"title":"Numerical Simulation of Jet Mixing in Supersonic Crossflow: Effect of Jet Exit Geometry","authors":"T. Iwasa, N. Tsuboi","doi":"10.2322/tjsass.65.172","DOIUrl":"https://doi.org/10.2322/tjsass.65.172","url":null,"abstract":"","PeriodicalId":54419,"journal":{"name":"Transactions of the Japan Society for Aeronautical and Space Sciences","volume":"1 1","pages":""},"PeriodicalIF":1.1,"publicationDate":"2022-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"68664545","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":4,"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
One Year On-Orbit Results of Improved Bus, LoRa Demonstration and Novel Backplane Mission of a 1U CubeSat Constellation 1U立方体卫星星座改进母线、LoRa论证和新型背板任务一年在轨结果
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.213
A. Maskey, Pooja Lepcha, H. Shrestha, Withanage Dulani Chamika, Tharindu Lakmal Dayarathna Malmadayalage, M. Kishimoto, Yuta Kakimoto, Yuji Sasaki, Turtogtokh Tumenjargal, G. Maeda, Sangkyun Kim, H. Masui, T. Yamauchi, M. Cho
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引用次数: 1
Feasibility Study of Controlling Supersonic Boundary-layer Flows Using Jets Flapping at Several Tens of Kilohertz 利用几十千赫兹扑动射流控制超音速边界层流动的可行性研究
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.221
Rui Aoki, Ikuhiro Fujimura, T. Handa, Chungil Lee, Y. Ozawa, Y. Saito, T. Nonomura, Keisuke Asai
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引用次数: 3
Abstracts of the Papers Published in Journal of the Japan Society for Aeronautical and Space Sciences (Vol. 70, No. 3, Jun. 2022) 《日本航空航天学会学报》(第70卷第3期,2022年6月)论文摘要
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.204
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引用次数: 0
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Transactions of the Japan Society for Aeronautical and Space Sciences
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