Publications
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…
NASA's Common Research Model (CRM) is the subject of numerous publications detailing its development, experimental investigations, and aerodynamic database. The model is designed for applied Computational Fluid Dynamics (CFD) validation studies, as explored in the AIAA-2008-6919 paper.
In 2010, an experimental investigation of the CRM was featured in the AIAA-2010-4218 paper, which was invited to present its findings. The 2011 series of papers delves deeper into the CRM's capabilities and performance.
In AIAA-2011-0878, the effects of active sting damping on CRM data quality are examined. The active sting damper's design and performance are detailed in AIAA-2011-0953.
The CRM's behavior in the NASA Langley National Transonic Facility and NASA Ames 11-Ft Transonic Wind Tunnel is analyzed in AIAA-2011-1126 and AIAA-2011-1127, respectively. These papers highlight the CRM's dynamic data and pressure-sensing capabilities.
The CRM's geometry, computational results, and ice accretion database are also covered in various publications, demonstrating the model's versatility and comprehensive approach to wind tunnel testing. The official CRM website offers more information for those interested in its full capabilities.
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