|
|
|
|||||||||||||||||||||||
|
|
||||||||||||||||||||||||
|
|
Computational fluid dynamics, usually abbreviated as CFD, is a branch of fluid mechanics that uses numerical methods and algorithms to solve and analyze problems that involve fluid flows. For many years, the study of dynamics, heat transfer, combustion, and fluid-structure interaction were unthinkable without the help of CFD, and this dependence has increased as more of the flow becomes amenable to numerical prediction. It is clear that CFD plays a significant role in the effective design, application, and performance evaluation of gas turbines and modern piping systems.
At Southwest Research Institute (SwRI), CFD is used comprehensively to solve turbomachinery fluid/thermal problems in tandem with experienced review staff and experimental verification of results. Its use in internal flow investigations is usually focused on examining phenomena such as:
Computational Fluid Dynamics Capabilities
SwRI maintains a variety of commercial and SwRI-developed analysis and computational codes to meet specific needs. Computational fluid dynamics is used along with other analysis, 1D modeling and a number of flow facilities to support simulations and understanding of fluid flows.
SwRI can offer you a full range of capabilities and experience in computational fluid dynamics, including becoming an extension of your engineering department. For more information about turbomachinery and piping system computational fluid dynamics at SwRI or how you can contract with SwRI, please contact Jeff Moore, Ph.D. at jmoore@swri.org or call (210) 522-5812.
|
|
||||||||||||||||||||||
|
| Fluids and Machinery Engineering Department | Mechanical Engineering Division | SwRI Home | |
||||||||||||||||||||||||
|
Southwest Research Institute® (SwRI®), headquartered in San Antonio, Texas, is a multidisciplinary, independent, nonprofit, applied engineering and physical sciences research and development organization with 11 technical divisions. |
||||||||||||||||||||||||
|
January 07, 2013 |
||||||||||||||||||||||||