Přejít k obsahu


Impact of Rapid Thermal Fluctuations of The Air Flow Into Engine Inlet To The Gas-Dynamics Stability of The Turbojet Engine

Citace: HOCKO, M., GÁŠPÁR, R. Impact of Rapid Thermal Fluctuations of The Air Flow Into Engine Inlet To The Gas-Dynamics Stability of The Turbojet Engine. In Power System Engineering, Thermodynamics and Fluid Flow. Plzeň: Západočeská univerzita v Plzni, 2013. s. 1-8. ISBN: 978-80-261-0230-4
Druh: STAŤ VE SBORNÍKU
Jazyk publikace: eng
Anglický název: Impact of Rapid Thermal Fluctuations of The Air Flow Into Engine Inlet To The Gas-Dynamics Stability of The Turbojet Engine
Rok vydání: 2013
Místo konání: Plzeň
Název zdroje: Západočeská univerzita v Plzni
Autoři: Ing. Marián Hocko PhD , Ing. Roman Gášpár
Abstrakt EN: The article deals with impact of rapid thermal fluctuations of the air flow into engine inlet to the gas-dynamics stability of the turbojet en-gine. Theoretical background of these processes, which causes many accidents in aviation, could be applied on operation stability of turbo-jet engines which are used as energetic units, cogeneration units or power units in many others transport vehicles.
Klíčová slova

Zpět

Patička