Abstract
This paper presents an early stage integration of propulsion system into multidisciplinary aircraft design process by accounting various types of drag forces generated by intake, engine and nozzle key parameters. An in-house code has been developed empirical formulas and will be supported by CFD analysis for inlet, engine and nozzle components. For engine uninstalled performance, F119-PW-100 like engine performance cycle deck modeled with Numerical Propulsion System Simulation (NPSS) software. For the intake, 2D caret type, fixed intake is considered and for the nozzle, 2D nozzle performance assumptions are used to calculate losses due to the installation of the propulsion system.
| Original language | English |
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| Title of host publication | AIAA Propulsion and Energy Forum, 2021 |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| ISBN (Print) | 9781624106118 |
| DOIs | |
| Publication status | Published - 2021 |
| Event | AIAA Propulsion and Energy Forum, 2021 - Virtual, Online Duration: 9 Aug 2021 → 11 Aug 2021 |
Publication series
| Name | AIAA Propulsion and Energy Forum, 2021 |
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Conference
| Conference | AIAA Propulsion and Energy Forum, 2021 |
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| City | Virtual, Online |
| Period | 9/08/21 → 11/08/21 |
Bibliographical note
Publisher Copyright:© 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.