NEGATIVE IMPACTS OF THE THERMAL AIR FLOW CHANGES ON THE TURBOJET ENGINE
Abstract
The article deals with impact of rapid thermal fluctuations of the air flow into engine inlet to the gas-dynamics stability of the turbojet engine. Theoretical background of these processes, which causes many accidents in aviation, could be applied on operation stability of turbojet engines which are used as energetic units, cogeneration units or power units in many others transport vehicles.
Keywords
compressor stall; turbojet engine; supply of stability work; non-stationary thermal field; unstable thermal field
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