Engine weight estimation of fifth generation fighter aircraft for high range and manoeuvrability
Küçük Resim Yok
Tarih
2020
Yazarlar
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
Inderscience Enterprises Ltd
Erişim Hakkı
info:eu-repo/semantics/closedAccess
Özet
This study focuses on afterburner turbofan engine weight estimation for fifth generation fighter aircrafts. Model developed in this study by investigating 26 engine cases categorised by the criteria the requirement of selection amongst to engines expected to be used in fifth generation fighter depend on four parameters with approximate to +/- 25% error. Technology level effect engine weight strongly so parameter reflect technology level is determined based on new technology engines used in fifth generation fighter aircraft by statistical method. Model reflect technology level is expected to be used in conceptual design stages of fifth generation fighter engine.
Açıklama
Anahtar Kelimeler
Fifth Fighter Aircraft, Thrust, Weight Ratio, Afterburner, Turbofan
Kaynak
International Journal Of Sustainable Aviation
WoS Q Değeri
Scopus Q Değeri
Cilt
6
Sayı
3
