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- W2182607680 abstract "Compressor is composed with the rotor and stator blades at each stage. Aerodynamic shapes of the blades play the major role to enhance the efficiency of the compressor in terms of the pressure ratio. In this work I want to focus on this blade’s geometry by changing various standard profiles like NACA and RAF (royal air force) to get the maximum output in terms to get the higher pressure ratio and number of stages which I want to reduce. ABSTRACT Basia P.R PG Student, L.D. College of Engineering, Ahmedabad" @default.
- W2182607680 created "2016-06-24" @default.
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- W2182607680 date "2013-01-01" @default.
- W2182607680 modified "2023-09-27" @default.
- W2182607680 title "CFD Analysis of the Multistage Axial Flowcompressor" @default.
- W2182607680 hasPublicationYear "2013" @default.
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