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@article{160280,
        author = {Rajni Verma and Dr. Rajesh Kumar Saluja},
        title = { OPTIMISED ENERGY MANAGEMENT OF HYBRID ELECTRIC PROPULSION},
        journal = {International Journal of Innovative Research in Technology},
        year = {},
        volume = {10},
        number = {1},
        pages = {87-96},
        issn = {2349-6002},
        url = {https://ijirt.org/article?manuscript=160280},
        abstract = {This research work focuses on the design and optimization of a hybrid-electric propulsion system for a small general aviation aircraft, Hyperion. The study aims to estimate aerodynamic data, performance parameters, and optimize the propulsion system to achieve maximum efficiency.The concept of hybrid-electric propulsion is introduced, highlighting its advantages over traditional propulsion systems. The estimated aerodynamic data and performance parameters are used to determine the optimal design of Hyperion, which includes a combination of electric and internal combustion engines.The Hyperion program is then discussed, which involves the implementation of the hybrid-electric propulsion system and testing of the aircraft. The results of the optimization process show that the hybrid-electric propulsion system significantly improves the aircraft's fuel efficiency and reduces its emissions.In conclusion, this study demonstrates the potential of hybrid-electric propulsion systems in general aviation aircraft. The implementation of such systems could lead to significant improvements in fuel efficiency and environmental sustainability in the aviation industry.},
        keywords = {optimization process; hybrid-electric propulsion system;  sustainability; aviation industry},
        month = {},
        }