Preliminary Assessment of Turbomachinery Codes

摘要: Summary and Recommendation A number of different CFD (computational fluid dynamics) codes have been developed used at NASA Glenn Research Center to evaluate turbomachinery aerodynamics thermal performance (table 1). These unique capabilities were by one or a group individual researchers Center. Several these are research having sparse documentation, making it challenging for other potential users understand the code methodology and/or run flow analysis. The usage can be drastically improved with proper documentation. One recommendation improve current situation is each developer develop comprehensive user manual train new about level that capable performing analyses codes. Potential future work commercial compare them simulation accuracy heat transfer.