Publications

28/08/2026 às 21:0815 Aufrufe
Front view of the Common Research Model in a wind tunnel.
Front view of the Common Research Model in a wind tunnel.
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This website is currently under construction.
Please see the full NASA Common Research Model website for current information.

High-Speed CRM Publications

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

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

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

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

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: Analysis of NASA Common Research Model Dynamic Data

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

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

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

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: Support System Effects on the NASA Common Research Model

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

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

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

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

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

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: Transonic Tail Buffet Simulations for the Common Research Model

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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