Title :
Effects of Circumferential Inlet Total-Pressure Distortion on a Compressor
Author_Institution :
Coll. of Energy & Power Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing
Abstract :
A program based on the parallel compressor is developed for the calculation of inlet total-pressure distortion on a compressor. The mixing of momentum, quality and energy is considered. Performance at four speed lines has been presented with 6% and 8% of distortion index by simulation. Results are reasonable and in line with the previous test.
Keywords :
compressors; circumferential inlet total-pressure distortion; distortion index; energy; momentum; parallel compressor; simulation; Analytical models; Automation; Concurrent computing; Educational institutions; Engines; Integral equations; Power engineering and energy; Power engineering computing; Pulse compression methods; Testing; compressor; inlet distortion; simulation;
Conference_Titel :
Computer and Automation Engineering, 2009. ICCAE '09. International Conference on
Conference_Location :
Bangkok
Print_ISBN :
978-0-7695-3569-2
DOI :
10.1109/ICCAE.2009.81
