@inproceedings{cee1c25d814644d09e513646a49414e0,
title = "Development of a Liquid Hydrogen Combustion Based High Bypass Geared Turbofan Model in NPSS",
abstract = "A Liquid Hydrogen (LH2) based combustion model in NPSS is developed for a conventional single aisle, twin engine subsonic commercial aircraft. This study describes the development of the engine model with N+3 technology parameters which is validated against published engine cycle data. The model is then used to run liquid hydrogen fuel in NPSS, and emissions calculations are performed based on engine emissions data for current technology level cycles. A full description of the emissions calculations is given as well as the performance comparison of conventional aviation jet fuel vs hydrogen.",
author = "Carter, {Richard E.} and Agarwal, {Ramesh K.}",
note = "Publisher Copyright: {\textcopyright} 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA AVIATION 2022 Forum ; Conference date: 27-06-2022 Through 01-07-2022",
year = "2022",
doi = "10.2514/6.2022-3431",
language = "English",
isbn = "9781624106354",
series = "AIAA AVIATION 2022 Forum",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA AVIATION 2022 Forum",
}