MATHEMATICAL MODEL FOR THE PREDICTION OF SINGLE-SPOOL TURBOJET ENGINE OFF-DESIGN PERFORMANCE (CROSBI ID 525956)
Prilog sa skupa u zborniku | izvorni znanstveni rad
Podaci o odgovornosti
Domitrović, Anita ; Bazijanac, Ernest ; Stojković, Vjekoslav
engleski
MATHEMATICAL MODEL FOR THE PREDICTION OF SINGLE-SPOOL TURBOJET ENGINE OFF-DESIGN PERFORMANCE
This paper analyses off-design performance of a turbojet engine. A mathematical model for calculation of single-spool turbojet engine off-design performance was developed. The model is based on the known on-design characteristic of the engine which is design for UAV (Unmanned Aerial Vehicle). Calculation results for a range of flight parameters and various throttle settings are presented for the known turbojet engine. The obtained off-design characteristics can be used for the prediction of engine performance in its future operation and for modeling the engine controls.
off-design performance ; single spool turbojet engine
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Podaci o prilogu
511-519.
2002.
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objavljeno
Podaci o matičnoj publikaciji
Proceedings of the First Symosium for Explosive Matherials, Weapons and Military Technology
Deskovski, Stojče ; Smileski, Rose
Ohrid: Military Academy ''General Mihailo Apostolski'', Skopje
Podaci o skupu
The First Symosium for Explosive Matherials, Weapons and Military Technology (with international participation)
predavanje
01.01.2002-01.01.2002
Ohrid, Sjeverna Makedonija