The Temperature and Material Distribution Inside a Gas Turbine Engine
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Tarih
2022
Yazarlar
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
Crimson Publishers
Erişim Hakkı
info:eu-repo/semantics/openAccess
Attribution-NonCommercial-NoDerivs 3.0 United States
Attribution-NonCommercial-NoDerivs 3.0 United States
Özet
The propulsion for the air vehicles is generated by the power obtained from the engines. Especially during take-off and climb phases, the air vehicles need the maximum power. Mainly, as presented in Figure 1, it is possible to handle the flight stages in 8 sections, 2 of which are runway maneuvers (Taxi). The cruise phase begins immediately after the climb phase is completed. In this stage, the fuel consumption is less than take-off and climb phases. Although it depends on the aircraft configuration and meteorological conditions, the descent phase, which usually takes place with a 3° nose angle, is one of the most critical stages. In this phase, the use of fuel is less than that of the cruise.
Açıklama
Anahtar Kelimeler
Gas turbine engine, Material distribution
Kaynak
Evolutions in Mechanical Engineering
WoS Q Değeri
Scopus Q Değeri
Cilt
4
Sayı
1