A conception of a two-combustor turbofan engine is the main scope of this paper. At the beginning, the problems of turbofan engines development are briefly discussed as a background of this work. In this part the turbofa...
The gas turbine engine has evolved rapidly during past decades to provide a reliable and efficient business solution for global transportation. The engine design process is clearly a large contributor to this evolution....
EP ID EP65362
DOI -
Views 92
Downloads 0
How To Cite
Maciej Krasiński, Andrzej Trojnacki (2013). OPTIMIZATION AND UNIFICATION
OF TWO-STAGE HELICAL GEAR REDUCER. Journal of KONES, 20(2),
213-219. https://europub.co.uk/articles/-A-65362
Sign In Europub
For faster login or register use your social account.
ATTEMPT OF INJECTORS FAILURE DETECTION BASED ON MEASUREMENT OF THE ANGULAR SPEED DISCRETE VALUE
POSSIBILITY OF REDUCING CO2 EMISSIONS FOR EXAMPLE ELECTRIC VEHICLES
EVALUATION ACCURACY OF COMBUSTION CHAMBER TIGHTNESS IN PISTON ENGINES, ON THE BASIS OF A DEVELOPED INDICATOR DIAGRAM
TWO-COMBUSTOR TURBOFAN ENGINE PERFORMANCE ANALYSIS
A conception of a two-combustor turbofan engine is the main scope of this paper. At the beginning, the problems of turbofan engines development are briefly discussed as a background of this work. In this part the turbofa...
MULTIDISCIPLINARY DESIGN AND OPTIMIZATION OF GAS TURBINE ENGINE LOW PRESSURE TURBINE AT PRELIMINARY DESIGN STAGE
The gas turbine engine has evolved rapidly during past decades to provide a reliable and efficient business solution for global transportation. The engine design process is clearly a large contributor to this evolution....