Matematički model primarne zone komore sagorevanja turbomlaznog motora
Mathematical model of turbojet engine combustion chamber primary zone
Apstrakt
Razvijen je i eksperimentalno potvrđen matematički model primarne zone komore sagorevanja turbomlaznog motora. Komora sagorevanja je prstenasta sa prstenastim jediničnim isparivačem postavljenim centralno u primarnu zonu. Ovakva konfiguracija je vrlo interesantna za aplikacije kod kojih su dominantni zahtevi za malim dimenzijama. Model je ispitivan u sklopu cele komore sagorevanja i ocenjivan je preko potpunosti sagorevanja cele komore.
Mathematical model of turbojet engine primary zone was developed and tested Combustion chamber was of annular type with single annular vaporizer positioned at the center. This configuration is very attractive for the applications where small dimensions are of primary interest. The model was tested as a part of combustion chamber and it was estimated through the overall combustion chamber efficiency.
Ključne reči:
vaporizer / turbojet / primary zone / combustion chamberIzvor:
FME Transactions, 2007, 35, 1, 29-34Izdavač:
- Univerzitet u Beogradu - Mašinski fakultet, Beograd
Kolekcije
Institucija/grupa
Mašinski fakultetTY - JOUR AU - Davidović, Nikola PY - 2007 UR - https://machinery.mas.bg.ac.rs/handle/123456789/725 AB - Razvijen je i eksperimentalno potvrđen matematički model primarne zone komore sagorevanja turbomlaznog motora. Komora sagorevanja je prstenasta sa prstenastim jediničnim isparivačem postavljenim centralno u primarnu zonu. Ovakva konfiguracija je vrlo interesantna za aplikacije kod kojih su dominantni zahtevi za malim dimenzijama. Model je ispitivan u sklopu cele komore sagorevanja i ocenjivan je preko potpunosti sagorevanja cele komore. AB - Mathematical model of turbojet engine primary zone was developed and tested Combustion chamber was of annular type with single annular vaporizer positioned at the center. This configuration is very attractive for the applications where small dimensions are of primary interest. The model was tested as a part of combustion chamber and it was estimated through the overall combustion chamber efficiency. PB - Univerzitet u Beogradu - Mašinski fakultet, Beograd T2 - FME Transactions T1 - Matematički model primarne zone komore sagorevanja turbomlaznog motora T1 - Mathematical model of turbojet engine combustion chamber primary zone EP - 34 IS - 1 SP - 29 VL - 35 UR - https://hdl.handle.net/21.15107/rcub_machinery_725 ER -
@article{ author = "Davidović, Nikola", year = "2007", abstract = "Razvijen je i eksperimentalno potvrđen matematički model primarne zone komore sagorevanja turbomlaznog motora. Komora sagorevanja je prstenasta sa prstenastim jediničnim isparivačem postavljenim centralno u primarnu zonu. Ovakva konfiguracija je vrlo interesantna za aplikacije kod kojih su dominantni zahtevi za malim dimenzijama. Model je ispitivan u sklopu cele komore sagorevanja i ocenjivan je preko potpunosti sagorevanja cele komore., Mathematical model of turbojet engine primary zone was developed and tested Combustion chamber was of annular type with single annular vaporizer positioned at the center. This configuration is very attractive for the applications where small dimensions are of primary interest. The model was tested as a part of combustion chamber and it was estimated through the overall combustion chamber efficiency.", publisher = "Univerzitet u Beogradu - Mašinski fakultet, Beograd", journal = "FME Transactions", title = "Matematički model primarne zone komore sagorevanja turbomlaznog motora, Mathematical model of turbojet engine combustion chamber primary zone", pages = "34-29", number = "1", volume = "35", url = "https://hdl.handle.net/21.15107/rcub_machinery_725" }
Davidović, N.. (2007). Matematički model primarne zone komore sagorevanja turbomlaznog motora. in FME Transactions Univerzitet u Beogradu - Mašinski fakultet, Beograd., 35(1), 29-34. https://hdl.handle.net/21.15107/rcub_machinery_725
Davidović N. Matematički model primarne zone komore sagorevanja turbomlaznog motora. in FME Transactions. 2007;35(1):29-34. https://hdl.handle.net/21.15107/rcub_machinery_725 .
Davidović, Nikola, "Matematički model primarne zone komore sagorevanja turbomlaznog motora" in FME Transactions, 35, no. 1 (2007):29-34, https://hdl.handle.net/21.15107/rcub_machinery_725 .