, scalability and ease-of-use of our CFD solver Cobalt on a variety of complex problems. Validation of the software through comparisons to experimental data is emphasized... and control characteristics of high-performance maneuverung aircraft with moving control surfaces. The purpose is to evaluate a computational approach using CFD and System... Identification Read more . Store Separation using Overset Capability This application presents recent results of the F-18C JDAM release first issued as a CFD challenge in 1998. The...

Characteristics of High-Performance Maneuvering Aircraft Using High-Resolution CFD Simulation with and without Moving Control Surfaces Jan 2013 Can Legacy Codes Scale on Tens of Thousands... Simulation Jun 2004 Role of the Barrel Shock as Control Element for Hypersonic Transverse Jet Injection Flows AIAA 2004-2698, Jun 2004 Summary of the 2004 CFD Validation Workshop... Understanding Abrupt Wing Stall With CFD AIAA 2003-0592, Jan 2003 Large and Detached Eddy Simulations of a Circular Cylinder Using Unstructured Grids AIAA 2003-0775, Jan 2003 Unsteady CFD...

Latest News Home First Time . Every Time Cobalt Solutions, LLC delivers advanced Computational Fluid Dynamics (CFD) analysis capabilities for a multitude of applications. To expand your...

. Typically, in-house R&D addresses the more fundamental aspects of CFD, while the end product of customer directed R&D tends to be a specific modeling capability previously...

Reynolds-averaged Navier Stokes (RANS) CFD calculations were fairly successful in predicting mean flow characteristics indicative of AWS, they failed to predict unsteady shock... Turning Goals into Reality award from NASA. Forsythe, J.R., Woodson, S.H., Unsteady CFD Calculations of Abrupt Wing Stall Using Detached-Eddy Simulation, AIAA 2003-0594, Jan 2003.... Woodson, S.H., Green, B.E., Chung, J.J., Grove, D.V., Parikh, P.C., Forsythe, J.R., Understanding Abrupt Wing Stall With CFD, AIAA 2003-0592, Jan 2003. Hall, R.M., Woodson, S.H...