This paper presents an analysis of the mechanism of compressor surge in a turbo-jet engine due to pressure disturbances at the air intake inlet. The computational model simulating the whole engine from the air intake to the exhaust nozzle, can predict surge hammer, as well as compressor surge cycles. The computed results show that a significant correlation exists between the compressor surge and the magnitude and duration of the pressure disturbances. (DePo)
A study on the mechanism of compressor surge due to inlet pressure disturbances
Studie des Mechanismuses von Verdichterstoerungen durch Stoerungen im Einlassdruck
AIAA-Papers ; 1-11
1978
11 Seiten, 16 Bilder, 17 Quellen
Aufsatz (Konferenz)
Englisch
Inlet dynamics and compressor surge
AIAA | 1969
|Inlet dynamics and compressor surge
AIAA | 1971
|