Vu, M.D. and Nguyen, K.T. and Dao, T.T. (2019) The Effect of Cooling-Air Flow Conditions on the Thermal State of High-Pressure Nozzle Blade. In: 2019 International Conference on System Science and Engineering, ICSSE 2019, 20 July 2019 through 21 July 2019.
The Effect of Cooling-Air Flow Conditions on the Thermal State of High-Pressure Nozzle Blade.pdf
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Abstract
Developing technique utilized for cooling turbine blades plays an important role in designing as well as manufacturing Gas Turbine Engine (GTE). This may enhance the GTE's lifetime and decrease its fuel consumption. The paper numerically examines the effect of cooling-Air mass flow rate and other flow conditions including temperature and pressure on the thermal state of high-pressure nozzle blade of the DR 76 gas turbine engine. © 2019 IEEE.
| Item Type: | Conference or Workshop Item (Paper) |
|---|---|
| Divisions: | Faculties > Faculty of Vehicle and Energy Engineering |
| Identification Number: | 10.1109/ICSSE.2019.8823110 |
| Uncontrolled Keywords: | Aircraft propulsion; Computational fluid dynamics; Cooling; Fuel consumption; Gas turbines; High pressure effects; Nozzles; Cooling air; Cooling air flow; Cooling turbine blades; Flow condition; GTE DR 76; High pressure; Temperature and pressures; Thermal state; Turbomachine blades |
| Additional Information: | Conference code: 151782. Language of original document: English. |
| URI: | http://eprints.lqdtu.edu.vn/id/eprint/9296 |
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