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This thesis investigates combining the three main components of an auxiliary power unit (APU) - the compressor, burner, and turbine - into a single centrifugal rotor. Equations describing the new turbomachinery cycle were developed using one-dimensional compressible flow principles. An optimization program called Model Center was used to obtain best design points for various cases. The results showed high specific power outputs without constraints, but unrealistic rotor sizes. With constraints to limit mate

Author

Tri Kurniawan

Language

EN