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    Incorporation of Electrical Systems Models Into an Existing Thermodynamic Cycle Code (2003)
    In:  CASI
    Details
    Publication Date: 2018-06-06
    Description: Integration of entire system includes: Fuel cells, motors, propulsors, thermal/power management, compressors, etc. Use of existing, pre-developed NPSS capabilities includes: 1) Optimization tools; 2) Gas turbine models for hybrid systems; 3) Increased interplay between subsystems; 4) Off-design modeling capabilities; 5) Altitude effects; and 6) Existing transient modeling architecture. Other factors inclde: 1) Easier transfer between users and groups of users; 2) General aerospace industry acceptance and familiarity; and 3) Flexible analysis tool that can also be used for ground power applications.
    Keywords: Aircraft Propulsion and Power
    Type: 2002 Computing and Interdisciplinary Systems Office Review and Planning Meeting; 63-71; NASA/TM-2003-211896
    Format: application/pdf
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