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SAE International Journal of Aerospace最新文献

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Parametric Studies on Airfoil-Boundary Layer Ingestion Propulsion System 翼型-边界层进气推进系统参数化研究
IF 0.4
SAE International Journal of Aerospace Pub Date : 2020-03-11 DOI: 10.4271/01-13-01-0003
M. El-Salamony, L. Teperin
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引用次数: 1
Understanding the Impact of Standardized SAE Waveform Parameter Variation on Artificial Lightning Plasma, Specimen Loading, and Composite Material Damage 了解标准化SAE波形参数变化对人工闪电等离子体、试样加载和复合材料损伤的影响
IF 0.4
SAE International Journal of Aerospace Pub Date : 2020-02-18 DOI: 10.4271/01-13-01-0002
S. Millen, A. Murphy, G. Abdelal, G. Catalanotti
{"title":"Understanding the Impact of Standardized SAE Waveform Parameter Variation on Artificial Lightning Plasma, Specimen Loading, and Composite Material Damage","authors":"S. Millen, A. Murphy, G. Abdelal, G. Catalanotti","doi":"10.4271/01-13-01-0002","DOIUrl":"https://doi.org/10.4271/01-13-01-0002","url":null,"abstract":"Previous works have established strategies to model artificial test lightning plasma with specific waveform parameters and use the predicted plasma behavior to estimate test specimen damage. To date no computational works have quantified the influence of varying the waveform parameters on the predicted plasma behavior and resulting specimen damage. Herein test standard Waveform B has been modelled and the waveform parameters of ‘waveform peak’, ‘rise time’ and ‘time to reach the post-peak value’ have been varied. The plasma and specimen behaviors have been modelled using the Finite Element (FE) method (a Magnetohydrodynamic FE multiphysics model for the plasma, a FE thermal-electric model for the specimen). For the test arrangements modelled herein it has been found that ‘peak current’ is the key parameter influencing plasma properties and specimen damage. A 10% increase in peak current magnitude (and resulting 21% increase in action integral) results in a 12% increase in plasma peak pressure, a 5% increase in specimen surface current density, and subsequently a 8.7% increase in thermal damage volume and a 15.2% increase in thermal damage depth. Overall action integral has the strongest correlation with four of the five considered damage measures. Peak current has the strongest correlation with the other damage measure.","PeriodicalId":44558,"journal":{"name":"SAE International Journal of Aerospace","volume":" ","pages":""},"PeriodicalIF":0.4,"publicationDate":"2020-02-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"48178781","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: 5
Mathematical Model of Heat-Controlled Accumulator (HCA) for Microgravity Conditions 微重力条件下热控蓄能器的数学模型
IF 0.4
SAE International Journal of Aerospace Pub Date : 2020-01-20 DOI: 10.4271/01-13-01-0001
G. Gorbenko, P. Koval, Konstantin Sergeevich Yepifanov, P. Gakal, Rustem Turna
{"title":"Mathematical Model of Heat-Controlled Accumulator (HCA) for\u0000 Microgravity Conditions","authors":"G. Gorbenko, P. Koval, Konstantin Sergeevich Yepifanov, P. Gakal, Rustem Turna","doi":"10.4271/01-13-01-0001","DOIUrl":"https://doi.org/10.4271/01-13-01-0001","url":null,"abstract":"","PeriodicalId":44558,"journal":{"name":"SAE International Journal of Aerospace","volume":"13 1","pages":"5-23"},"PeriodicalIF":0.4,"publicationDate":"2020-01-20","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"48348054","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: 4
Conceptual Design, Material, and Structural Optimization of a Naval Fighter Nose Landing Gear for the Estimated Static Loads 海军战斗机前起落架的概念设计、材料和结构优化
IF 0.4
SAE International Journal of Aerospace Pub Date : 2019-12-13 DOI: 10.4271/01-12-02-0009
Swagata Paul, K. Suresh, C. Kumar
{"title":"Conceptual Design, Material, and Structural Optimization of a Naval Fighter Nose Landing Gear for the Estimated Static Loads","authors":"Swagata Paul, K. Suresh, C. Kumar","doi":"10.4271/01-12-02-0009","DOIUrl":"https://doi.org/10.4271/01-12-02-0009","url":null,"abstract":"","PeriodicalId":44558,"journal":{"name":"SAE International Journal of Aerospace","volume":"12 1","pages":"175-187"},"PeriodicalIF":0.4,"publicationDate":"2019-12-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"45951055","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
Multicriteria Optimization, Sensitivity Analysis, and Prediction of Bond Characteristics of Vacuum Diffusion Bonded Aero Engine Ti6Al4V Alloy Joints 航空发动机Ti6Al4V合金真空扩散焊接头键合特性多准则优化、灵敏度分析及预测
IF 0.4
SAE International Journal of Aerospace Pub Date : 2019-12-13 DOI: 10.4271/01-12-02-0008
T. Pragatheswaran, S. Rajakumar, V. Balasubramanian, S. Kavitha, V. Petley, S. Verma
{"title":"Multicriteria Optimization, Sensitivity Analysis, and Prediction of Bond Characteristics of Vacuum Diffusion Bonded Aero Engine Ti6Al4V Alloy Joints","authors":"T. Pragatheswaran, S. Rajakumar, V. Balasubramanian, S. Kavitha, V. Petley, S. Verma","doi":"10.4271/01-12-02-0008","DOIUrl":"https://doi.org/10.4271/01-12-02-0008","url":null,"abstract":"","PeriodicalId":44558,"journal":{"name":"SAE International Journal of Aerospace","volume":"12 1","pages":"153-174"},"PeriodicalIF":0.4,"publicationDate":"2019-12-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"47852344","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: 3
Stall Mitigation and Lift Enhancement of NACA 0012 with Triangle-Shaped Surface Protrusion at a Reynolds Number of 105 雷诺数为105时具有三角形表面突起的NACA 0012的失速缓解和升力增强
IF 0.4
SAE International Journal of Aerospace Pub Date : 2019-11-21 DOI: 10.4271/01-12-02-0007
A. Bodavula, R. Yadav, U. Guven
{"title":"Stall Mitigation and Lift Enhancement of NACA 0012 with Triangle-Shaped Surface Protrusion at a Reynolds Number of 105","authors":"A. Bodavula, R. Yadav, U. Guven","doi":"10.4271/01-12-02-0007","DOIUrl":"https://doi.org/10.4271/01-12-02-0007","url":null,"abstract":"","PeriodicalId":44558,"journal":{"name":"SAE International Journal of Aerospace","volume":"12 1","pages":"133-151"},"PeriodicalIF":0.4,"publicationDate":"2019-11-21","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"48983528","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: 3
Improving the Modelling of Dissociating Hydrogen Nozzles 改进离解氢喷嘴的建模
IF 0.4
SAE International Journal of Aerospace Pub Date : 2019-11-21 DOI: 10.4271/01-12-02-0006
A. Boretti
{"title":"Improving the Modelling of Dissociating Hydrogen Nozzles","authors":"A. Boretti","doi":"10.4271/01-12-02-0006","DOIUrl":"https://doi.org/10.4271/01-12-02-0006","url":null,"abstract":"","PeriodicalId":44558,"journal":{"name":"SAE International Journal of Aerospace","volume":"12 1","pages":"117-132"},"PeriodicalIF":0.4,"publicationDate":"2019-11-21","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"43850229","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
Enhancing Flight Path Separation to Reduce Bird Strikes with Ultraviolet Radiation 加强航路间隔以减少紫外线辐射对鸟的撞击
IF 0.4
SAE International Journal of Aerospace Pub Date : 2019-10-29 DOI: 10.4271/01-12-02-0005
D. Ronning
{"title":"Enhancing Flight Path Separation to Reduce Bird Strikes with Ultraviolet Radiation","authors":"D. Ronning","doi":"10.4271/01-12-02-0005","DOIUrl":"https://doi.org/10.4271/01-12-02-0005","url":null,"abstract":"","PeriodicalId":44558,"journal":{"name":"SAE International Journal of Aerospace","volume":" ","pages":""},"PeriodicalIF":0.4,"publicationDate":"2019-10-29","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"44055183","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
Design and Experiment on Aircraft Electromechanical Actuator Fan at Different Altitudes and Rotational Speeds 飞机机电致动器风机在不同高度和转速下的设计与试验
IF 0.4
SAE International Journal of Aerospace Pub Date : 2019-06-07 DOI: 10.4271/01-12-01-0003
Wei Wu, Yeong-Ren Lin, E. Gyasi, J. Kizito, Q. Leland, L. Chow
{"title":"Design and Experiment on Aircraft Electromechanical Actuator Fan at Different Altitudes and Rotational Speeds","authors":"Wei Wu, Yeong-Ren Lin, E. Gyasi, J. Kizito, Q. Leland, L. Chow","doi":"10.4271/01-12-01-0003","DOIUrl":"https://doi.org/10.4271/01-12-01-0003","url":null,"abstract":"","PeriodicalId":44558,"journal":{"name":"SAE International Journal of Aerospace","volume":"1 1","pages":""},"PeriodicalIF":0.4,"publicationDate":"2019-06-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.4271/01-12-01-0003","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"70622571","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: 3
Process Regulations and Mechanism of WEDM of Combustor Material 燃烧材料电火花线切割的工艺规律及机理
IF 0.4
SAE International Journal of Aerospace Pub Date : 2019-06-07 DOI: 10.4271/01-12-01-0004
Bhupinder Singh, J. P. Misra
{"title":"Process Regulations and Mechanism of WEDM of Combustor Material","authors":"Bhupinder Singh, J. P. Misra","doi":"10.4271/01-12-01-0004","DOIUrl":"https://doi.org/10.4271/01-12-01-0004","url":null,"abstract":"","PeriodicalId":44558,"journal":{"name":"SAE International Journal of Aerospace","volume":"1 1","pages":""},"PeriodicalIF":0.4,"publicationDate":"2019-06-07","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.4271/01-12-01-0004","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"42472659","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: 5
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