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Schlieren Visualization and Motion Analysis of an Isolated and Clustered Particle(s) after Interacting with Planar Shock 与平面激波相互作用后孤立和聚集粒子的纹影可视化和运动分析
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.185
T. Nagata, T. Nonomura, K. Ohtani, Keisuke Asai
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引用次数: 2
Landing Point Analysis and Forecast Wind Data Validation for Low-Ballistic-Coefficient Flight Vehicles with a Deployable Aeroshell 低弹道系数可展开飞行器着陆点分析及预测风数据验证
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.244
Yasunori Nagata, Kazuhiko Yamada, Tatsuro Nakao
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引用次数: 0
The Effect of Discharge Mode on Ion Energy and Plasma Potential in the Plume Plasma Region 放电方式对羽流等离子体区离子能量和等离子体势的影响
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.1
Shun Imai, Daisuke Imaguchi, Hiroki Watanabe, K. Kubota, Shinatora Cho, Y. Oshio, I. Funaki
The ion energy angle distribution and its relationship to plasma parameters for spot and plume modes are elucidated for a LaB 6 hollow cathode with a radiative heater. Measurements were conducted using a retarding potential analyzer (RPA) and a single Langmuir probe. The ion energy distribution function (IEDF) characteristics showed di ff erent tendencies in the current density and mass fl ow-rate dependence under di ff erent plasma modes. The IEDF peak potential for the spot mode varied from 16 to 23V with increasing current density, and the IEDF peak potential for the plume mode varied from 16 to 32V with decreasing mass fl ow rate. Considering angle dependency of ion energy, when the observation angle was changed from the radial direction to the axial direction, the IEDF peak potential increased from 29 to 40V for the plume mode (10A, 10sccm) and increased slightly from 16 to 18V for the spot mode (20A, 30sccm). The probe measurement analysis revealed that the IEDF peak energies are the same as, or exceed, the plasma potential and have a qualitative correlation with the electron temperature spatial distribution.
本文研究了带辐射加热器的lab6空心阴极在斑点和羽流模式下的离子能量角分布及其与等离子体参数的关系。测量使用延迟电位分析仪(RPA)和单个朗缪尔探针进行。在不同的等离子体模式下,离子能量分布函数(IEDF)特性在电流密度和质量流率依赖方面表现出不同的趋势。随着电流密度的增大,斑点模式的IEDF峰值电位在16 ~ 23V之间变化;随着质量流量的减小,羽流模式的IEDF峰值电位在16 ~ 32V之间变化。考虑到离子能量的角度依赖性,当观测角度从径向转向轴向时,羽流模式(10A, 10sccm)的IEDF峰值电位从29 v增加到40V,斑模式(20A, 30sccm)的IEDF峰值电位从16 v略微增加到18V。探针测量分析表明,IEDF峰值能量与等离子体势相同或超过等离子体势,并与电子温度空间分布有定性的相关性。
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引用次数: 1
Dynamically Extendable Chords with Non-Harmonic Motions to Improve the Performance of Variable-Speed Tail Rotors 带非谐波运动的动态扩展弦提高变速尾桨性能
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.253
Haoyun Wan, D. Han, Yuhang Zhang
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引用次数: 0
Abstracts of the Papers Published in Journal of the Japan Society for Aeronautical and Space Sciences (Vol. 70, No. 5, Oct. 2022) 《日本航空航天学会学报》(第70卷第5期,2022年10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.65.273
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引用次数: 0
Numerical/Experimental Hybrid Study on Base Pressure and Cavity Pressure Corrections for Transonic Wind Tunnel Tests 跨声速风洞试验中基腔压力修正的数值/实验混合研究
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.116
H. Kawashima, K. Kitamura, S. Nonaka
{"title":"Numerical/Experimental Hybrid Study on Base Pressure and Cavity Pressure Corrections for Transonic Wind Tunnel Tests","authors":"H. Kawashima, K. Kitamura, S. Nonaka","doi":"10.2322/tjsass.65.116","DOIUrl":"https://doi.org/10.2322/tjsass.65.116","url":null,"abstract":"","PeriodicalId":54419,"journal":{"name":"Transactions of the Japan Society for Aeronautical and Space Sciences","volume":"69 1","pages":""},"PeriodicalIF":1.1,"publicationDate":"2022-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"68664236","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: 1
Fuel Efficiency Prediction Model to Enhance the Fuel Efficiency and Reduce the Carbon Emissions 提高燃油效率,减少碳排放的燃油效率预测模型
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.237
Show-Ling Jang, Y. Cho, J. Yoo, K. Yoo
{"title":"Fuel Efficiency Prediction Model to Enhance the Fuel Efficiency and Reduce the Carbon Emissions","authors":"Show-Ling Jang, Y. Cho, J. Yoo, K. Yoo","doi":"10.2322/tjsass.65.237","DOIUrl":"https://doi.org/10.2322/tjsass.65.237","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":"68664821","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
Abstracts of the Papers Published in Journal of the Japan Society for Aeronautical and Space Sciences (Vol. 70, No. 2, Apr. 2022) 《日本航空航天学会学报》(第70卷第2期,2022年4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.65.138
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引用次数: 0
Flap Usage Considering Swirl Velocities to Reduce the Download on a Winged Helicopter in Hover 考虑旋涡速度的旋翼直升机在悬停状态下减少下载的襟翼使用
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.195
Shunsaku Arita, Noriaki Itoga, Ryoya Hayashi
{"title":"Flap Usage Considering Swirl Velocities to Reduce the Download on a Winged Helicopter in Hover","authors":"Shunsaku Arita, Noriaki Itoga, Ryoya Hayashi","doi":"10.2322/tjsass.65.195","DOIUrl":"https://doi.org/10.2322/tjsass.65.195","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":"68664719","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
Experimental Investigation of Free-to-Roll Motion of a Blunt-Nosed Slender Body Configuration 钝鼻细长体构型自由滚转运动的实验研究
IF 1.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2022-01-01 DOI: 10.2322/tjsass.65.205
Z. Qi, Li Zhao, Yankui Wang
{"title":"Experimental Investigation of Free-to-Roll Motion of a Blunt-Nosed Slender Body Configuration","authors":"Z. Qi, Li Zhao, Yankui Wang","doi":"10.2322/tjsass.65.205","DOIUrl":"https://doi.org/10.2322/tjsass.65.205","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":"68664918","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
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Transactions of the Japan Society for Aeronautical and Space Sciences
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