Experimental Analysis on the Operating Line of Two Gas Turbine Engines by Testing with Different Exhaust Nozzle Geometries
This paper presents a special analysis study about the gas turbine operating line, and an overall description of a gas turbines project, based on experimental data from two particular applications, in order to convert two different types of aero engines into the same engine configuration. The experi...
Main Authors: | Razvan Marius Catana, Gabriel Petre Badea |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2023-07-01
|
Series: | Energies |
Subjects: | |
Online Access: | https://www.mdpi.com/1996-1073/16/15/5627 |
Similar Items
-
Parametric design and IR signature study of exhaust plume from elliptical-shaped exhaust nozzles of a low flying UAV using CFD approach
by: Fazal Haq, et al.
Published: (2022-03-01) -
Effect of a Secondary Injection on the Performance of Three-Dimensional Over-under TBCC Exhaust Nozzles
by: H. Yang, et al.
Published: (2023-01-01) -
Studies and Experimental Research in the Evaluation of TV2-117A Turboshaft Engine Working Regimes
by: Răzvan Marius Catană, et al.
Published: (2022-04-01) -
Experimental study on the nozzle-shape effect on liquid jet characteristics in gaseous crossflow
by: B. Jalili, et al.
Published: (2023-11-01) -
Gas flow in nozzles/
by: 410253 Pirumov, U. G., et al.
Published: (1986)