Özet
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.
| Orijinal dil | İngilizce |
|---|---|
| Ana bilgisayar yayını başlığı | AIAA Propulsion and Energy Forum, 2021 |
| Yayınlayan | American Institute of Aeronautics and Astronautics Inc, AIAA |
| ISBN (Basılı) | 9781624106118 |
| DOI'lar | |
| Yayın durumu | Yayınlandı - 2021 |
| Etkinlik | AIAA Propulsion and Energy Forum, 2021 - Virtual, Online Süre: 9 Ağu 2021 → 11 Ağu 2021 |
Yayın serisi
| Adı | AIAA Propulsion and Energy Forum, 2021 |
|---|
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| ???event.eventtypes.event.conference??? | AIAA Propulsion and Energy Forum, 2021 |
|---|---|
| Şehir | Virtual, Online |
| Periyot | 9/08/21 → 11/08/21 |
Bibliyografik not
Publisher Copyright:© 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Finansman
The three authors would like to thank the NATO STO AVT-333 (Integration of Propulsion, Power, and Thermal Subsystem Models into Air Vehicle Conceptual Design) research task group for their collaboration. The first author would also like to thank Turkish Aerospace Industry for the support for this paper.
| Finansörler | Finansör numarası |
|---|---|
| Turkish Aerospace Industry | |
| North Atlantic Treaty Organization | STO AVT-333 |