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48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)最新文献

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Large Eddy Simulation of Continuously Adjustable Hypersonic Wind Tunnel 连续可调高超声速风洞大涡模拟
48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.) Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3545
Jesse R. Maxwell, Gabriel B. Goodwin
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引用次数: 1
An adaptive timestepping algorithm for particle time integration in coupled CFD-DEM simulations. 耦合CFD-DEM模拟中粒子时间积分的自适应时间步进算法。
48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.) Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3715
H. Sitaraman, R. Grout
{"title":"An adaptive timestepping algorithm for particle time integration in coupled CFD-DEM simulations.","authors":"H. Sitaraman, R. Grout","doi":"10.2514/6.2018-3715","DOIUrl":"https://doi.org/10.2514/6.2018-3715","url":null,"abstract":"","PeriodicalId":93061,"journal":{"name":"48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)","volume":"25 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"82385298","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: 1
Resonance Start-up in a Rectangular Cavity 矩形谐振腔的谐振启动
48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.) Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3871
Aaron M. Turpin, Daniel Y. Chin, J. L. Hill, Kenneth Granlund
{"title":"Resonance Start-up in a Rectangular Cavity","authors":"Aaron M. Turpin, Daniel Y. Chin, J. L. Hill, Kenneth Granlund","doi":"10.2514/6.2018-3871","DOIUrl":"https://doi.org/10.2514/6.2018-3871","url":null,"abstract":"","PeriodicalId":93061,"journal":{"name":"48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)","volume":"33 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"76528784","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: 1
CFD Analysis of Heterogeneous and Homogeneous Multi-Truck Platoon Aerodynamic Drag Reduction 非均匀与均匀多车排气动减阻CFD分析
48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.) Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3862
Michael Siemon, D. Nichols
{"title":"CFD Analysis of Heterogeneous and Homogeneous Multi-Truck Platoon Aerodynamic Drag Reduction","authors":"Michael Siemon, D. Nichols","doi":"10.2514/6.2018-3862","DOIUrl":"https://doi.org/10.2514/6.2018-3862","url":null,"abstract":"","PeriodicalId":93061,"journal":{"name":"48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)","volume":"75 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"76197820","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
Drag Decomposition Using Partial Pressure Fields in the Compressible Navier-Stokes Equations 可压缩Navier-Stokes方程中分压场的阻力分解
48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.) Pub Date : 2018-06-24 DOI: 10.2514/6.2018-2908
S. Schmitz
{"title":"Drag Decomposition Using Partial Pressure Fields in the Compressible Navier-Stokes Equations","authors":"S. Schmitz","doi":"10.2514/6.2018-2908","DOIUrl":"https://doi.org/10.2514/6.2018-2908","url":null,"abstract":"The static-pressure field in the steady and compressible Navier–Stokes equations is decomposed into Euler (inviscid) and dissipative (viscous) partial-pressure fields as a generalization of the inc...","PeriodicalId":93061,"journal":{"name":"48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)","volume":"19 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"87451354","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
An Overset Generalized Minimal Residual Method for the Multi-Solver Paradigm in Helios. Helios中多求解器范式的超集广义最小残差法。
48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.) Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3247
D. Jude, J. Sitaraman, V. Lakshminarayan, J. Baeder
{"title":"An Overset Generalized Minimal Residual Method for the Multi-Solver Paradigm in Helios.","authors":"D. Jude, J. Sitaraman, V. Lakshminarayan, J. Baeder","doi":"10.2514/6.2018-3247","DOIUrl":"https://doi.org/10.2514/6.2018-3247","url":null,"abstract":"","PeriodicalId":93061,"journal":{"name":"48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)","volume":"24 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"88408436","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
Simultaneous PSP and surface deformation measurements for fluid-structure interactions in a shock tube 激波管内流固相互作用的同步PSP和表面变形测量
48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.) Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3870
K. Lynch, E. Jones, J. Wagner
{"title":"Simultaneous PSP and surface deformation measurements for fluid-structure interactions in a shock tube","authors":"K. Lynch, E. Jones, J. Wagner","doi":"10.2514/6.2018-3870","DOIUrl":"https://doi.org/10.2514/6.2018-3870","url":null,"abstract":"","PeriodicalId":93061,"journal":{"name":"48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)","volume":"31 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"86769849","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: 8
Boundary Layer Transition (BOLT) Flight Experiment Overview 边界层过渡(BOLT)飞行实验综述
48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.) Pub Date : 2018-06-24 DOI: 10.2514/6.2018-2892
Bradley M. Wheaton, Dennis C. Berridge, T. Wolf, Ryan T. Stevens, B. McGrath
{"title":"Boundary Layer Transition (BOLT) Flight Experiment Overview","authors":"Bradley M. Wheaton, Dennis C. Berridge, T. Wolf, Ryan T. Stevens, B. McGrath","doi":"10.2514/6.2018-2892","DOIUrl":"https://doi.org/10.2514/6.2018-2892","url":null,"abstract":"","PeriodicalId":93061,"journal":{"name":"48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)","volume":"67 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"79221764","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: 30
Numerical Analysis of Laminar and Turbulent Shock-Wave Boundary Layer Interactions 层流和湍流激波边界层相互作用的数值分析
48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.) Pub Date : 2018-06-24 DOI: 10.2514/6.2018-4033
A. Gross, Sunyoung Lee
{"title":"Numerical Analysis of Laminar and Turbulent Shock-Wave Boundary Layer Interactions","authors":"A. Gross, Sunyoung Lee","doi":"10.2514/6.2018-4033","DOIUrl":"https://doi.org/10.2514/6.2018-4033","url":null,"abstract":"","PeriodicalId":93061,"journal":{"name":"48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)","volume":"5 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"87448781","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: 7
Using Adaptive Mesh Refinement to Study Grid Resolution Effects for Shock-Boundary Layer Interactions 利用自适应网格细化研究激波边界层相互作用下网格分辨率的影响
48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.) Pub Date : 2018-06-24 DOI: 10.2514/6.2018-3858
M. E. Olsen, Randolph P. Lillard
{"title":"Using Adaptive Mesh Refinement to Study Grid Resolution Effects for Shock-Boundary Layer Interactions","authors":"M. E. Olsen, Randolph P. Lillard","doi":"10.2514/6.2018-3858","DOIUrl":"https://doi.org/10.2514/6.2018-3858","url":null,"abstract":"Adaptive Mesh Refinement (AMR) promises a much more computationally efficient means to obtain a discrete approximation to a continuous boundary value problem of a specified accuracy than classic isotropic grid refinement. The AMR capability of OVERFLOW is utilized to provide estimates of the exact analytical solutions to problems of interest for turbulence modeling. Predictions of surface pressure and skin friction, essentially the state of stress at the surface, shows little difference with grids believed to be “grid resolved.” Velocity profiles, on the other hand, show marked differences in flows with shocks. The AMR method, as implemented in OVERFLOW 2.2k, appears to provide the ability to produce arbitrarily accurate solutions at a predictable cost much smaller than classic uniform mesh refinement.","PeriodicalId":93061,"journal":{"name":"48th AIAA Fluid Dynamics Conference 2018 : held at the AIAA Aviation Forum 2018 : Atlanta, Georgia, USA, 25-29 June 2018. AIAA Fluid Dynamics Conference (48th : 2018 : Atlanta, Ga.)","volume":"7 1","pages":""},"PeriodicalIF":0.0,"publicationDate":"2018-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"91254693","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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