Multiply Connected Cavity Flows in Turbomachines
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Published: 1996
Total Pages: 18
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DOWNLOAD EBOOKChanging any one component in a set of multiply connected cavities, such as the compressor discharge seal, causes flow changes throughout the entire engine. T-70O engine test data and numerical simulations of the space shuttle main engine high-pressure fuel turbopump, the four stage T-56/501D turbine, and swirl brake dynamics are cited as examples. The needs for time-dependent optimization of turbine and compressor flow fields, for use of seals to enhance rotor stability, for predictive maintenance, and for a clean-sheet approach to engine design are concluded.