DocumentCode :
3091307
Title :
Analysis of 3D Numerical Simulation for an Airfoil Probe in a Compressor
Author :
Luo, Ju
Author_Institution :
Coll. of Energy & Power Eng., Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
Volume :
2
fYear :
2009
fDate :
28-30 Dec. 2009
Firstpage :
560
Lastpage :
562
Abstract :
A numerical simulation has been done using CFX11.0 to study the effect of an airfoil probe installed at the leading edge of first stage stator in a compressor. Combination of structured and unstructured grids has been used during the calculation. Result shows that blade loading with and without probe is obviously different at 50% height of blade, while the effect at 20% and 80% height of blade is not obvious. The result has proved that probe indeed has an effect on performance of a compressor, and especially on a compressor with a high speed, high pressure ratio. A corresponding test will be done to validate the result and for a further study.
Keywords :
aerodynamics; aerospace components; aerospace engines; blades; compressors; computational fluid dynamics; numerical analysis; stators; 3D numerical simulation; CFX11.0; airfoil probe; aviation engines; blade loading; compressor; first stage stator; unstructured grids; Automotive components; Numerical simulation; Probes; airfoil probe; compressor; numerical simulation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer and Electrical Engineering, 2009. ICCEE '09. Second International Conference on
Conference_Location :
Dubai
Print_ISBN :
978-1-4244-5365-8
Electronic_ISBN :
978-0-7695-3925-6
Type :
conf
DOI :
10.1109/ICCEE.2009.280
Filename :
5380225
Link To Document :
بازگشت