出版物

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This website is currently under construction.

请参阅完整的美国国家航天局（NASA）通用研究模型网站以获取最新信息。

Please see the full NASA Common Research Model website for current information.

高速CRM出版物

High-Speed CRM Publications

AIAA-2008-6919：应用计算流体力学（CFD）验证研究中通用研究模型的开发

AIAA-2008-6919: Development of a Common Research Model for Applied CFD Validation Studies

AIAA-2010-4218：美国国家航天局通用研究模型的实验研究（特邀）

AIAA-2010-4218: Experimental Investigation of the NASA Common Research Model (Invited)

AIAA-2011-0878：主动尾刺阻尼对通用研究模型数据质量的影响

AIAA-2011-0878: Effects of Active Sting Damping on Common Research Model Data Quality

AIAA-2011-0953：美国国家航天局通用研究模型主动尾刺阻尼器的设计与性能

AIAA-2011-0953: Design and Performance of an Active Sting Damper for the NASA Common Research Model

AIAA-2011-1126：美国国家航天局通用研究模型在美国国家航天局兰利国家跨声速设施和美国国家航天局艾姆斯11英尺跨声速风洞中的实验研究（特邀）

AIAA-2011-1126: Experimental Investigations of the NASA Common Research Model in the NASA Langley National Transonic Facility and NASA Ames 11-Ft Transonic Wind Tunnel (Invited)

AIAA-2011-1127：美国国家航天局通用研究模型动态数据分析

AIAA-2011-1127: Analysis of NASA Common Research Model Dynamic Data

AIAA-2011-1128：美国国家航天局11英尺跨声速风洞中美国国家航天局通用研究模型的压敏漆测量

AIAA-2011-1128: Pressure-Sensitive Paint Measurements on the NASA Common Research Model in the NASA 11-ft Transonic Wind Tunnel

AIAA-2011-1129：通用研究模型上测量与计算的蒙皮摩擦分布比较

AIAA-2011-1129: A Comparison of the Measured and Computed Skin Friction Distribution on the Common Research Model

AIAA-2011-3508：第五届AIAA计算流体力学阻力预测研讨会中关于通用研究模型翼/身组合的统一基准网格（特邀）

AIAA-2011-3508: A Unified Baseline Grid about the Common Research Model Wing/Body for the Fifth AIAA CFD Drag Prediction Workshop (Invited)

AIAA-2011-3699：日本航天局（JAXA）对美国国家航天局通用研究模型模拟的远场阻力分析

AIAA-2011-3699: Far-Field Drag Analysis of NASA Common Research Model Simulations by JAXA

NASA-TM-2011-217065：在国家跨声速设施进行的第197号测试中，关于通用研究模型的压敏漆测试结果

NASA-TM-2011-217065: Results From a Pressure Sensitive Paint Test Conducted at the National Transonic Facility on Test 197: The Common Research Model

AIAA-2012-0707：支承系统对美国国家航天局通用研究模型的影响

AIAA-2012-0707: Support System Effects on the NASA Common Research Model

AIAA-2012-3209：对美国国家航天局通用研究模型支承系统影响和翼扭转的进一步研究

AIAA-2012-3209: Further Investigation of the Support System Effects and Wing Twist on the NASA Common Research Model

AIAA-2013-0052：使用美国国家航天局通用研究模型（CRM）风洞数据的网格评估

AIAA-2013-0052: Grid Assessment Using the NASA Common Research Model (CRM) Wind Tunnel Data

AIAA-2013-0493：日本航天局在相对较低雷诺数下进行的80%缩比美国国家航天局通用研究模型风洞测试

AIAA-2013-0493: 80% Scaled NASA Common Research Model Wind Tunnel Test at JAXA at Relatively Low Reynolds Number

AIAA-2013-0495：日本航天局风洞测试中美国国家航天局通用研究模型动态数据的分析

AIAA-2013-0495: Analysis of NASA Common Research Model Dynamic Data in JAXA Wind Tunnel Tests

AIAA-2013-0871：通过在欧洲跨声速风洞（ETW）中使用美国国家航天局CRM模型，进行实验与数值非定常尾流分析及壁宿干扰评估

AIAA-2013-0871:Going For Experimental and Numerical Unsteady Wake Analyses Combined with Wall Interference Assessment by Using the NASA CRM Model in ETW

AIAA-2013-0963：日本航天局美国国家航天局通用研究模型风洞测试的壁宿和支承系统干扰修正

AIAA-2013-0963: Wall and Support Interference Corrections of NASA Common Research Model Wind Tunnel Tests in JAXA

AIAA-2013-2509：第五届AIAA计算流体力学阻力预测研讨会中，流固耦合和湍流模型对德国航空航天中心（DLR）结果影响的研究

AIAA-2013-2509: Investigation of Fluid-Structure-Coupling and Turbulence Model Effects on the DLR Results of the Fifth AIAA CFD Drag Prediction Workshop

AIAA-2013-2510：通用研究模型的跨声速尾宿抖振模拟

AIAA-2013-2510: Transonic Tail Buffet Simulations for the Common Research Model

AIAA-2014-0251：将气动弹性扭转纳入双发美国国家航天局通用研究模型的计算流体力学分析

AIAA-2014-0251: Inclusion of Aeroelastic Twist into the CFD Analysis of the Twin-Engine NASA Common Research Model

AIAA-2014-0567：基于雷诺平均纳维-斯托克斯方程（RANS）的通用研究模型翼型气动外形优化研究

AIAA-2014-0567: RANS-based Aerodynamic Shape Optimization Investigations of the Common Research Model Wing

AIAA-2014-0598：通过新型材料和结构配置对美国国家航天局通用研究模型进行气动弹性剪裁

AIAA-2014-0598: Aeroelastic Tailoring of the NASA Common Research Model via Novel Material and Structural Configurations

AIAA-2014-0634：通用研究模型机翼的航空结构水平集拓扑优化

AIAA-2014-0634: Aerostructural Level Set Topology Optimization for a Common Research Model Wing

AIAA-2014-3135：美国国家航天局通用研究模型在国家跨声速设施（NTF）利用主动尾刺阻尼进行的测试包线张宿

AIAA-2014-3135:NASA Common Research Model Test Envelope Extension with Active Sting Damping at NTF

AIAA-2014-3171：湍流模型修正对美国国家航天局通用研究模型阻力预测的影响

AIAA-2014-3171: The Effects of Turbulence Model Corrections on Drag Prediction of NASA Common Research Model

AIAA-2014-3274：通用研究模型配置的航空结构优化

AIAA-2014-3274:Aerostructural optimization of the Common Research Model configuration

NASA TM-2014-218516：通用研究模型翼盒气动弹性剪裁的材料与厚度分级

NASA TM-2014-218516: Material and Thickness Grading for Aeroelastic Tailoring of the Common Research Model Wing Box

AIAA-2015-0264：通用研究模型机翼的多点气动外形优化研究

AIAA-2015-0264: Multipoint Aerodynamic Shape Optimization Investigations of the Common Research Model Wing

AIAA-2015-1093：美国国家航天局通用研究模型欧洲跨声速风洞测试数据与美国国家航天局测试数据的比较

AIAA-2015-1093: Comparison of the NASA Common Research Model European Transonic Wind Tunnel Test Data to NASA Test Data

AIAA-2015-1237：涡流发生器对二维和三维美国国家航天局通用研究模型影响的实验研究

AIAA-2015-1237: Experimental Investigation of Vortex Generator Effect on Two- and Three-Dimensional NASA Common Research Models

AIAA-2015-1718：通用研究模型翼-身-尾宿配置的气动外形优化

AIAA-2015-1718: Aerodynamic Shape Optimization of the Common Research Model Wing-Body-Tail Configuration

NASA-TM-2015-218697：用于气动弹性剪裁的通用研究模型翼盒内部结构设计

NASA-TM-2015-218697: Internal Structural Design of the Common Research Model Wing Box for Aeroelastic Tailoring

AIAA-2016-0308：高升力通用研究模型的开发：一种具有代表性的跨声速运输机高升力配置

AIAA-2016-0308: Development of the High Lift Common Research Model: A Representative High Lift Configuration for Transonic Transports

AIAA-2016-0939：未变形通用研究模型的大规模柔度最小化与屈曲拓扑优化

AIAA-2016-0939: Large-Scale Compliance-Minimization and Buckling Topology Optimization of the Undeformed Common Research Model

AIAA-2016-2023：美国国家航天局通用研究模型上跨声速格子玻尔兹曼方法的验证

AIAA-2016-2023: Validation of a Transonic Lattice-Boltzmann Method on the NASA Common Research Model

AIAA-2016-3431：第六届AIAA计算流体力学阻力预测研讨会的美国国家航天局通用研究模型

AIAA-2016-3431: NASA’s Common Research Model for the Sixth AIAA CFD Drag Prediction Workshop

AIAA-2016-3486：美国国家航天局通用研究模型：几何处理视角

AIAA-2016-3486: The NASA Common Research Model: A Geometry-Handling Perspective

AIAA-2016-3655：低速条件下风洞支承系统对美国国家航天局通用研究模型的影响

AIAA-2016-3655: Wind Tunnel Support System Influence on NASA Common Research Model at Low Speed Conditions

AIAA-2016-4044：美国国家航天局通用研究模型跨声速抖振的非定常压力测量

AIAA-2016-4044: Unsteady Pressure Measurement of Transonic Buffet on NASA Common Research Model

AIAA-2017-0319：用于风洞测试的高升力通用研究模型：主动流动控制视角

AIAA-2017-0319: High Lift Common Research Model for Wind Tunnel Testing: An Active Flow Control Perspective

AIAA-2017-0320：使用USM3D和FUN3D求解器对高升力通用研究模型进行的计算流体力学分析

AIAA-2017-0320:Computational Fluid Dynamic Analyses for the High Lift Common Research Model Using the USM3D and FUN3D Solvers

AIAA-2017-0363：美国国家航天局高升力通用研究模型的网格生成

AIAA-2017-0363: Mesh Generation for the NASA High Lift Common Research Model

AIAA-2017-0964：法国国家航空航天研究中心（ONERA）S1MA风洞中通用研究模型的实验研究——与阻力预测研讨会（DPW）数值结果的比较

AIAA-2017-0964: Experimental Investigations on the Common Research Model at ONERA-S1MA – Comparison with DPW Numerical Results

AIAA-2017-3362：高升力通用研究模型的噪声模拟

AIAA-2017-3362: Noise Simulations of the High-Lift Common Research Model

AIAA-2017-4145：美国国家航天局通用研究模型的航空结构优化

AIAA-2017-4145: Aero-Structural Optimization of the NASA Common Research Model

AIAA-2017-4233：使用不同湍流模型对美国国家航天局通用研究模型进行阻力预测

AIAA-2017-4233:Drag Prediction of NASA Common Research Models Using Different Turbulence Models

AIAA-2017-4235：使用带有壁宿函数的浸入边界法对美国国家航天局通用研究模型进行湍流模拟

AIAA-2017-4235:Turbulent Flow Simulations of the NASA Common Research Model using the Immersed Boundary Method with a Wall Function

AIAA-2017-4292：CREATE-AV Kestrel双网格对美国国家航天局通用研究模型的模拟

AIAA-2017-4292:CREATETM-AV Kestrel Dual-Mesh Simulations of the NASA Common Research Model

AIAA-2017-4456：未偏转通用研究模型（uCRM）：用于研究大纵横比运输机机翼的航空结构模型

AIAA-2017-4456:Undeflected Common Research Model (uCRM): An Aerostructural Model for the Study of High Aspect Ratio Transport Aircraft Wings

AIAA-2018-0543：通过块结构笛卡尔网格对美国国家航天局通用研究模型进行的空气动力学分析

AIAA-2018-0543: Aerodynamic Analysis of NASA Common Research Model by Block-Structured Cartesian Mesh

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