Abstract
Results of an experimental study of the thermal state of a combined turbofan rotor consisting of a peripheral turbine stage and a central fan stage are reported. In particular, attention is given to the effect of gas temperature, air flow rate, and rotation speed on temperature distributions at characteristic points of the rotor. The relative dimensionless temperatures of the turbofan rotor are shown to be constant under all the regimes investigated. An approximate method is proposed for calculating the temperature of the rotor elements, and the results of calculations are compared with experimental data.
Citation Formats
Bileka, B D, Diachenko, A M, and Orinichev, I S.
Thermal state of a turbofan rotor.
Ukraine: N. p.,
1988.
Web.
Bileka, B D, Diachenko, A M, & Orinichev, I S.
Thermal state of a turbofan rotor.
Ukraine.
Bileka, B D, Diachenko, A M, and Orinichev, I S.
1988.
"Thermal state of a turbofan rotor."
Ukraine.
@misc{etde_7146486,
title = {Thermal state of a turbofan rotor}
author = {Bileka, B D, Diachenko, A M, and Orinichev, I S}
abstractNote = {Results of an experimental study of the thermal state of a combined turbofan rotor consisting of a peripheral turbine stage and a central fan stage are reported. In particular, attention is given to the effect of gas temperature, air flow rate, and rotation speed on temperature distributions at characteristic points of the rotor. The relative dimensionless temperatures of the turbofan rotor are shown to be constant under all the regimes investigated. An approximate method is proposed for calculating the temperature of the rotor elements, and the results of calculations are compared with experimental data.}
journal = []
volume = {10:2}
journal type = {AC}
place = {Ukraine}
year = {1988}
month = {Jan}
}
title = {Thermal state of a turbofan rotor}
author = {Bileka, B D, Diachenko, A M, and Orinichev, I S}
abstractNote = {Results of an experimental study of the thermal state of a combined turbofan rotor consisting of a peripheral turbine stage and a central fan stage are reported. In particular, attention is given to the effect of gas temperature, air flow rate, and rotation speed on temperature distributions at characteristic points of the rotor. The relative dimensionless temperatures of the turbofan rotor are shown to be constant under all the regimes investigated. An approximate method is proposed for calculating the temperature of the rotor elements, and the results of calculations are compared with experimental data.}
journal = []
volume = {10:2}
journal type = {AC}
place = {Ukraine}
year = {1988}
month = {Jan}
}