1. Add model for when twin scroll volute is used
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2. Incorporate secondary flows, including Agile link to AxCent
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3. Add convergent-divergent nozzle modeling
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4. Account for variable inlet inclination angle for mixed flow turbines
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5. Allow for preliminary calculations of mechanical properties (e.g. mass, inertia, and CG)
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6. Add running solver status for analysis mode (i.e. for real gas map generation)
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7. Add preliminary thrust calculations
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