Energy, exergy, thermoecologic, environmental, enviroeconomic and sustainability analyses and assessments of the aircraft engine fueled with biofuel and jet fuel. [PDF]
Akdeniz HY, Balli O, Caliskan H.
europepmc +1 more source
The endurance tests of the aeronautical equipment components by mathematical statistics application
The endurance test results of two representative components of turbojet engine are analysed using methods of mathematical statistics. The first test is related to endurance of the fuel pump, and the second one to the micropumps investigations. Researches
Dragoljub Vujić
doaj +1 more source
Self-teaching digital-computer program for fail-operational control of a turbojet engine in a sea-level test stand [PDF]
The design and evaluation are described of a digital turbojet engine control which is capable of sensing catastrophic failures in either the engine rotor speed or the compressor discharge static-pressure signal and is capable of switching control modes ...
Arpasi, D. J., Wallhagen, R. E.
core +1 more source
Unsteady flow characteristic analysis of turbine based combined cycle (TBCC) inlet mode transition
A turbine based combined cycle (TBCC) propulsion system uses a turbine-based engine to accelerate the vehicle from takeoff to the mode transition flight condition, at which point, the propulsion system performs a “mode transition” from the turbine to ...
Jun Liu, Huacheng Yuan, Guo Rongwei
doaj +1 more source
TRANSIENT PERFORMANCE OF A SINGLE-SPOOL TURBOJET ENGINE
The transient performance (acceleration and deceleration) analysis of turbojet gas turbine engire has been carried out in the present work. Transient simulation of the engines is based on the compatibility of flow and rotational speed but not of work ...
Arkan K. Al-Tael +2 more
doaj +1 more source
Analysis of Limitations Imposed on One-Spool Turbojet-Engine Designs by Turbines Having Downstream Stators at 0, 2.0, and 2.8 Flight Mach Numbers [PDF]
Limitations on turbojet engine design by turbines with downstream ...
Cavicchi, R. H., Constantine, A. B.
core +2 more sources
FSI Application in the Parametric Analysis of Blade-Disc Connection of Turbojet Engine Compressor
Olga Grzejszczak, Adam Kozakiewicz
openalex +2 more sources
Optimized modeling of energy and environmental metrics of mixed flow turbofan engine used regional aircraft. [PDF]
Uçar UU, Aygun H, Tanyeri B.
europepmc +1 more source
Comparison of numerical simulation results of the mixing chamber with physical experiment data
The mixing chamber of a turbojet engine is the object of the study. The thermogasdynamic processes in the mixing chamber of the turbojet engine before the turbine of the turbofan attachment are the subjects of the study.
Illia Yudin
doaj +1 more source
Turbine for ordnance turbojet engine. 2: Cold-air performance with opened stator [PDF]
A single-stage axial-flow turbine was investigated to determine the effect of increased stator throat area on the performance level of a turbojet engine turbine.
Haas, J. E. +2 more
core +1 more source

