AIAA Aviation 2019 Forum最新文献

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A wall function approach to account for rough surface heat transfer in Spalart-Allmaras turbulence model 考虑Spalart-Allmaras湍流模型中粗糙表面传热的壁函数方法
AIAA Aviation 2019 Forum Pub Date : 2019-06-17 DOI: 10.2514/6.2019-2918
Aviral Prakash, E. Laurendeau
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引用次数: 1
Level Set Topology Optimization for Design Dependent Pressure Loads: A Comparison Between FEM and RKPM 设计相关压力载荷的水平集拓扑优化:FEM与RKPM的比较
AIAA Aviation 2019 Forum Pub Date : 2019-06-17 DOI: 10.2514/6.2019-3559
A. Neofytou, R. Picelli, Jiun-Shyan Chen, H. Kim
{"title":"Level Set Topology Optimization for Design Dependent Pressure Loads: A Comparison Between FEM and RKPM","authors":"A. Neofytou, R. Picelli, Jiun-Shyan Chen, H. Kim","doi":"10.2514/6.2019-3559","DOIUrl":"https://doi.org/10.2514/6.2019-3559","url":null,"abstract":"","PeriodicalId":384114,"journal":{"name":"AIAA Aviation 2019 Forum","volume":"48 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-06-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121769305","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
Power Management Optimization for Off-Design Performance Assessment of Ducted Electric Fan with Boundary Layer Ingestion 边界层进气风管电风扇非设计性能评估的电源管理优化
AIAA Aviation 2019 Forum Pub Date : 2019-06-17 DOI: 10.2514/6.2019-3451
Joseph A. Brucculeri, Luis Salas Nunez, Jonathan C. Gladin, D. Mavris
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引用次数: 1
Automatic Generation of Numerical Methods for Time Integration in Large-Scale MDO 大规模MDO时间积分数值方法的自动生成
AIAA Aviation 2019 Forum Pub Date : 2019-06-17 DOI: 10.2514/6.2019-3664
Victor E. Gandarillas, John T. Hwang
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引用次数: 0
Flight Trajectory Optimization of a Sailplane after Rope Break during Tow-Assisted Takeoff 滑翔机拖曳起飞断绳后的飞行轨迹优化
AIAA Aviation 2019 Forum Pub Date : 2019-06-17 DOI: 10.2514/6.2019-2818
Armando R. Collazo Garcia, P. Ranjan, K. James, Phillip J. Ansell
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引用次数: 0
Consideration of Control Effector Dynamics and Saturations in an Extended INDI Approach 扩展INDI方法中控制效应器动力学和饱和度的考虑
AIAA Aviation 2019 Forum Pub Date : 2019-06-17 DOI: 10.2514/6.2019-3267
Stefan A. Raab, Jiannan Zhang, P. Bhardwaj, F. Holzapfel
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引用次数: 14
Aircraft Reserve Fuel Study with High-fidelity Fuel Approximation Model 基于高保真燃料近似模型的飞机储备燃料研究
AIAA Aviation 2019 Forum Pub Date : 2019-06-17 DOI: 10.2514/6.2019-3509
Yuan Lyu, Jefry Yanto, R. Liem
{"title":"Aircraft Reserve Fuel Study with High-fidelity Fuel Approximation Model","authors":"Yuan Lyu, Jefry Yanto, R. Liem","doi":"10.2514/6.2019-3509","DOIUrl":"https://doi.org/10.2514/6.2019-3509","url":null,"abstract":"","PeriodicalId":384114,"journal":{"name":"AIAA Aviation 2019 Forum","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-06-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130080960","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: 2
Comparison between RANS and hybrid RANS/LES simulations of jet/vortex interaction 射流/涡相互作用的RANS与混合RANS/LES模拟的比较
AIAA Aviation 2019 Forum Pub Date : 2019-06-17 DOI: 10.2514/6.2019-3405
Vivien Chmielarski, W. Ghedhaifi, E. Montreuil, A. Loseille
{"title":"Comparison between RANS and hybrid RANS/LES simulations of jet/vortex interaction","authors":"Vivien Chmielarski, W. Ghedhaifi, E. Montreuil, A. Loseille","doi":"10.2514/6.2019-3405","DOIUrl":"https://doi.org/10.2514/6.2019-3405","url":null,"abstract":"","PeriodicalId":384114,"journal":{"name":"AIAA Aviation 2019 Forum","volume":"21 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-06-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133912798","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
Wind Tunnel Testing of Active Flow Control on the High Lift Common Research Model 大扬程通用模型主动流控风洞试验研究
AIAA Aviation 2019 Forum Pub Date : 2019-06-17 DOI: 10.2514/6.2019-3723
John C. H. Lin, L. Melton, Judith A. Hannon, Marlyn Y. Andino, M. Koklu, K. Paschal, V. Vatsa
{"title":"Wind Tunnel Testing of Active Flow Control on the High Lift Common Research Model","authors":"John C. H. Lin, L. Melton, Judith A. Hannon, Marlyn Y. Andino, M. Koklu, K. Paschal, V. Vatsa","doi":"10.2514/6.2019-3723","DOIUrl":"https://doi.org/10.2514/6.2019-3723","url":null,"abstract":"A 10%-scale high-lift version of the Common Research Model (CRM-HL) and an Active Flow Control (AFC) version of the model equipped with a simple-hinged flap (CRM-SHLAFC) were successfully tested. The tests were performed in the 14by 22-Foot Subsonic Tunnel (14x22) at the NASA Langley Research Center (LaRC). The CRM-HL has a set of 37° inboard and outboard single-element Fowler flaps. The CRM-SHL-AFC has a set of 50° inboard and 55° outboard simple-hinged flaps equipped with integrated modular AFC cartridges on the flap shoulder. Both high-lift configurations share the same 30° slats and engine nacelle. Three new types of AFC devices were examined: the Double-Row Sweeping Jets (DRSWJ), the Alternating Pulsed Jets (APJ), and the High Efficiency Low Power (HELP) actuators. The DRSWJ and the APJ actuators used two rows of unsteady jets, whereas the HELP actuators used a combination of unsteady and steady jets, to overcome strong adverse pressure gradients while minimizing the mass flow usage. Nozzle pressure ratio, mass flow consumption and the power coefficient, which takes account of both supply air pressure and mass flow usage for the actuators, were used for judging the performance efficiency of the AFC devices. A prestall lift performance degradation for the CRM-HL configuration was resolved with a properly placed nacelle chine. The configuration with nacelle chine was chosen as the representative reference conventional high-lift case for comparison with the CRMSHL-AFC. The AFC-induced lift coefficient increment (DCL) was maintained for the entire lift curve over the CRM-SHL-AFC case with no AFC for almost all flow-control cases examined. The lift curve of the reference CRM-HL have a slightly steeper slope compared to those of the CRM-SHL-AFC configurations. The HELP actuation concept was extremely effective in controlling flow separation in the “linear region” of the curves comparing lift coefficient to mass flow rate. The HELP actuation achieved a targeted DCL of 0.50 using a moderate amount of mass flow and supply air pressure. The CRM-SHL-AFC configuration equipped with HELP actuation was able to match or exceed the lift performance of the reference conventional high-lift configuration (i.e., CRM-HL equipped with a nacelle chine), thus meeting the NASA Advanced Air Transport Technology (AATT) project goal.","PeriodicalId":384114,"journal":{"name":"AIAA Aviation 2019 Forum","volume":"10 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-06-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"129408377","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: 24
The Aerodynamics of a Civil Transport in Aerial Firefighting 空中灭火民用运输机的空气动力学
AIAA Aviation 2019 Forum Pub Date : 2019-06-17 DOI: 10.2514/6.2019-3697
Daniel Varner, L. K. Kliment, K. Rokhsaz
{"title":"The Aerodynamics of a Civil Transport in Aerial Firefighting","authors":"Daniel Varner, L. K. Kliment, K. Rokhsaz","doi":"10.2514/6.2019-3697","DOIUrl":"https://doi.org/10.2514/6.2019-3697","url":null,"abstract":"","PeriodicalId":384114,"journal":{"name":"AIAA Aviation 2019 Forum","volume":"3 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-06-17","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130704150","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
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