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This paper demonstrates a methodology whereby flight performance, mission analysis, and energy sizing concepts are generalized and combined with explicit consideration of vehicle trim and geometry parameterization within a vehicle sizing and performance analysis framework intended for novel vehicle configuration and propulsion system architectures.

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This page is a summary of: Generalized Energy-Based Flight Vehicle Sizing and Performance Analysis Methodology, Journal of Aircraft, December 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c036101.
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