|
|
|
|
|
Grigore Cican, Tiberius-Florian Frigioescu, Daniel-Eugeniu Crunteanu and Laurentiu Cristea
This paper explores the implementation of an ejector to a micro turbojet engine and analysis of the advantages in terms of acoustic and thrust/fuel consumption. Starting with the analytical equations and a series of numerical simulations, the optimal eje...
ver más
|
|
|
|
|
|
|
|
|
|
|
Razvan Nicoara, Daniel Crunteanu and Valeriu Vilag
As a main component of most gas-turbine engines, the axial flow turbines have been in a process of continuous improvement, reaching high efficiencies and reliability. A well-known drawback of these systems is the rapid decrease in performance when operat...
ver más
|
|
|
|
|
|
|
|
|
|
|
Razvan Edmond Nicoara, Daniel Eugeniu Crunteanu and Valeriu Alexandru Vilag
Extensively used in modern gas turbine engines in various applications, ranging from aerospace, marine and terrestrial propulsion to power generation and gas pumping, the axial flow turbines have been continuously updated and are now capable of high perf...
ver más
|
|
|
|
|
|
|
|
|
|
|
Palego, C.; Pothier, A.; Crunteanu, A.; Chatras, M.; Blondy, P.; Champeaux, C.; Tristant, P.; Catherinot, A
Pág. 729 - 735
|
|
|
|
|
|
|
|
|
|
|
Lacroix, B.; Pothier, A.; Crunteanu, A.; Cibert, C.; Dumas-Bouchiat, F.; Champeaux, C.; Catherinot, A.; Blondy, P.
Pág. 1314 - 1321
|
|
|
|
|
|