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Issue No. 06 - November/December (2007 vol. 9)
ISSN: 1521-9615
pp: 12-17
Allan van de Wall , GE Transportation-Aircraft Engines
Fu-Lin Tsung , GE Transportation-Aircraft Engines
Steven E. Gorrell , US Air Force Research Laboratory
ABSTRACT
Applying computational science and engineering to the design and analysis of high-performance compressors makes it possible to understand unsteady flow effects in gas turbine engines. Simulations have produced numerical data of greatly improved geometric, physical, and numerical fidelity than previously possible, helping next-generation engines achieve unprecedented performance.
INDEX TERMS
high-performance computing, HPC, gas turbines, jet engines, computational fluid dynamics, CFD, flow fields
CITATION
Allan van de Wall, Fu-Lin Tsung, Steven E. Gorrell, "Understanding Unsteady Flow Features in Transonic Compressors", Computing in Science & Engineering, vol. 9, no. , pp. 12-17, November/December 2007, doi:10.1109/MCSE.2007.130
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