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International Journal of Aeronautical and Space Sciences最新文献

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Numerical Evaluation of Varying Combustion Chamber Length on the Performance of Pulse Detonation Engine Using DES Model 利用 DES 模型对不同燃烧室长度对脉冲引爆发动机性能的影响进行数值评估
IF 1.7 4区 工程技术
International Journal of Aeronautical and Space Sciences Pub Date : 2024-05-23 DOI: 10.1007/s42405-024-00746-0
Arvind Pallela, Shivam Kumar, A. K. Thakur, Lovi Raj Gupta, Rajesh Singh
{"title":"Numerical Evaluation of Varying Combustion Chamber Length on the Performance of Pulse Detonation Engine Using DES Model","authors":"Arvind Pallela, Shivam Kumar, A. K. Thakur, Lovi Raj Gupta, Rajesh Singh","doi":"10.1007/s42405-024-00746-0","DOIUrl":"https://doi.org/10.1007/s42405-024-00746-0","url":null,"abstract":"","PeriodicalId":48819,"journal":{"name":"International Journal of Aeronautical and Space Sciences","volume":null,"pages":null},"PeriodicalIF":1.7,"publicationDate":"2024-05-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141106689","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
Comparison of Test Results and Finite-Element Analysis Using Elastoplastic Modeling of 2.5D C/SiC Composites 使用 2.5D C/SiC 复合材料弹塑性建模的测试结果与有限元分析的比较
IF 1.7 4区 工程技术
International Journal of Aeronautical and Space Sciences Pub Date : 2024-05-23 DOI: 10.1007/s42405-024-00729-1
Byoungchan Chae, Y. Ko
{"title":"Comparison of Test Results and Finite-Element Analysis Using Elastoplastic Modeling of 2.5D C/SiC Composites","authors":"Byoungchan Chae, Y. Ko","doi":"10.1007/s42405-024-00729-1","DOIUrl":"https://doi.org/10.1007/s42405-024-00729-1","url":null,"abstract":"","PeriodicalId":48819,"journal":{"name":"International Journal of Aeronautical and Space Sciences","volume":null,"pages":null},"PeriodicalIF":1.7,"publicationDate":"2024-05-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141104148","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
Firing Command Generation for Close-In Weapon System to Intercept High-Speed Targets 为拦截高速目标的近距离武器系统生成射击指令
IF 1.7 4区 工程技术
International Journal of Aeronautical and Space Sciences Pub Date : 2024-05-23 DOI: 10.1007/s42405-024-00743-3
Boseok Kim, Chang-Hun Lee
{"title":"Firing Command Generation for Close-In Weapon System to Intercept High-Speed Targets","authors":"Boseok Kim, Chang-Hun Lee","doi":"10.1007/s42405-024-00743-3","DOIUrl":"https://doi.org/10.1007/s42405-024-00743-3","url":null,"abstract":"","PeriodicalId":48819,"journal":{"name":"International Journal of Aeronautical and Space Sciences","volume":null,"pages":null},"PeriodicalIF":1.7,"publicationDate":"2024-05-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141106568","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
A Wind Speed Forecasting Method Based on Machine Learning for Operating Unguided Submunitions from a Cluster Munition 基于机器学习的风速预测方法，用于操作集束弹药中的非制导子弹药
IF 1.7 4区 工程技术
International Journal of Aeronautical and Space Sciences Pub Date : 2024-05-22 DOI: 10.1007/s42405-024-00751-3
Sung Jin Lee, Sang Gon Kim, Chan Gyu Kim, Cheong Hee Park
{"title":"A Wind Speed Forecasting Method Based on Machine Learning for Operating Unguided Submunitions from a Cluster Munition","authors":"Sung Jin Lee, Sang Gon Kim, Chan Gyu Kim, Cheong Hee Park","doi":"10.1007/s42405-024-00751-3","DOIUrl":"https://doi.org/10.1007/s42405-024-00751-3","url":null,"abstract":"","PeriodicalId":48819,"journal":{"name":"International Journal of Aeronautical and Space Sciences","volume":null,"pages":null},"PeriodicalIF":1.7,"publicationDate":"2024-05-22","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141111468","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
High-Fidelity Simulation and Performance Analysis of Twin-Spool Turbofan Engine Based on Multi-dynamics Approach 基于多动力学方法的双涡管涡扇发动机高保真模拟与性能分析
IF 1.7 4区 工程技术
International Journal of Aeronautical and Space Sciences Pub Date : 2024-05-18 DOI: 10.1007/s42405-024-00748-y
Chaochao Guo, Youchao Sun, Longbiao Li, Xiaodong Zhu
{"title":"High-Fidelity Simulation and Performance Analysis of Twin-Spool Turbofan Engine Based on Multi-dynamics Approach","authors":"Chaochao Guo, Youchao Sun, Longbiao Li, Xiaodong Zhu","doi":"10.1007/s42405-024-00748-y","DOIUrl":"https://doi.org/10.1007/s42405-024-00748-y","url":null,"abstract":"","PeriodicalId":48819,"journal":{"name":"International Journal of Aeronautical and Space Sciences","volume":null,"pages":null},"PeriodicalIF":1.7,"publicationDate":"2024-05-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"141125128","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
Prediction of Aircraft Departure/Spin Characteristics by Improving Kalviste Decomposing and Weak Nonlinear Analysis Method 通过改进卡尔维斯特分解法和弱非线性分析法预测飞机起飞/旋转特性
IF 1.7 4区 工程技术
International Journal of Aeronautical and Space Sciences Pub Date : 2024-04-22 DOI: 10.1007/s42405-024-00735-3
Lianghui Tu, Chao Yan, Xingyu Liu, Yuhao Wang, Yang Yang
{"title":"Prediction of Aircraft Departure/Spin Characteristics by Improving Kalviste Decomposing and Weak Nonlinear Analysis Method","authors":"Lianghui Tu, Chao Yan, Xingyu Liu, Yuhao Wang, Yang Yang","doi":"10.1007/s42405-024-00735-3","DOIUrl":"https://doi.org/10.1007/s42405-024-00735-3","url":null,"abstract":"","PeriodicalId":48819,"journal":{"name":"International Journal of Aeronautical and Space Sciences","volume":null,"pages":null},"PeriodicalIF":1.7,"publicationDate":"2024-04-22","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"140676957","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
Feasibility and Effectiveness of a Higher Harmonic Control System for a Medium Utility Helicopter 中型通用直升机高次谐波控制系统的可行性和有效性
IF 1.7 4区 工程技术
International Journal of Aeronautical and Space Sciences Pub Date : 2024-04-22 DOI: 10.1007/s42405-024-00736-2
Do-Hyung Kim, Jae-Sang Park, Shin-Won Bang
{"title":"Feasibility and Effectiveness of a Higher Harmonic Control System for a Medium Utility Helicopter","authors":"Do-Hyung Kim, Jae-Sang Park, Shin-Won Bang","doi":"10.1007/s42405-024-00736-2","DOIUrl":"https://doi.org/10.1007/s42405-024-00736-2","url":null,"abstract":"","PeriodicalId":48819,"journal":{"name":"International Journal of Aeronautical and Space Sciences","volume":null,"pages":null},"PeriodicalIF":1.7,"publicationDate":"2024-04-22","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"140678065","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
Design Procedure of a Variable Rectangular Inlet for TBCC Engine Considering Mass Flow Requirements 考虑质量流量要求的 TBCC 发动机可变矩形进气口设计程序
IF 1.7 4区 工程技术
International Journal of Aeronautical and Space Sciences Pub Date : 2024-04-22 DOI: 10.1007/s42405-024-00725-5
Young Jin Kim, H. Lee, Bok Jik Lee
{"title":"Design Procedure of a Variable Rectangular Inlet for TBCC Engine Considering Mass Flow Requirements","authors":"Young Jin Kim, H. Lee, Bok Jik Lee","doi":"10.1007/s42405-024-00725-5","DOIUrl":"https://doi.org/10.1007/s42405-024-00725-5","url":null,"abstract":"","PeriodicalId":48819,"journal":{"name":"International Journal of Aeronautical and Space Sciences","volume":null,"pages":null},"PeriodicalIF":1.7,"publicationDate":"2024-04-22","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"140676021","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
Steady-State Combustion Characteristics of a Pentad Impinging-Jet Injector Using Green Hypergolic Propellant 使用绿色过醇推进剂的五边形撞击喷射器的稳态燃烧特性
IF 1.7 4区 工程技术
International Journal of Aeronautical and Space Sciences Pub Date : 2024-04-18 DOI: 10.1007/s42405-024-00734-4
M. Shin, J. Oh, J. Cha, Y. Ko
{"title":"Steady-State Combustion Characteristics of a Pentad Impinging-Jet Injector Using Green Hypergolic Propellant","authors":"M. Shin, J. Oh, J. Cha, Y. Ko","doi":"10.1007/s42405-024-00734-4","DOIUrl":"https://doi.org/10.1007/s42405-024-00734-4","url":null,"abstract":"","PeriodicalId":48819,"journal":{"name":"International Journal of Aeronautical and Space Sciences","volume":null,"pages":null},"PeriodicalIF":1.7,"publicationDate":"2024-04-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"140690171","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
Static Mechanical Characteristics Analysis of Aircraft Tire Under Extreme Weather Conditions 极端天气条件下飞机轮胎的静态机械特性分析
IF 1.7 4区 工程技术
International Journal of Aeronautical and Space Sciences Pub Date : 2024-04-17 DOI: 10.1007/s42405-024-00719-3
Kai Lei, Jingtao Wu, Zhanpeng Ren, Wenliang Deng, Cong Wang
{"title":"Static Mechanical Characteristics Analysis of Aircraft Tire Under Extreme Weather Conditions","authors":"Kai Lei, Jingtao Wu, Zhanpeng Ren, Wenliang Deng, Cong Wang","doi":"10.1007/s42405-024-00719-3","DOIUrl":"https://doi.org/10.1007/s42405-024-00719-3","url":null,"abstract":"","PeriodicalId":48819,"journal":{"name":"International Journal of Aeronautical and Space Sciences","volume":null,"pages":null},"PeriodicalIF":1.7,"publicationDate":"2024-04-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"140693135","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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