NASA NTRS · 19870001767
Aerothermal modeling program, phase 2
Abstract
The accuracy and utility of current aerothermal models for gas turbine combustors must be improved. Three areas of concern are identified: improved numerical methods for turbulent viscous recirculating flows; flow interaction; and fuel injector-air swirl characterization. Progress in each area is summarized.
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Mularz, E. J.. 1984-10-01. Aerothermal modeling program, phase 2. https://ntrs.nasa.gov/citations/19870001767
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