A Method for designing transonic compressor blade propiles

Anbarasu, M and Pai, BR (1990) A Method for designing transonic compressor blade propiles. Project Report. National Aerospace Laboratories, Bangalore.

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A computer code is developed for rapid design of profiles suitable for transonic, highly loaded axial flow compressors . Analysis of the profiles derived from the procedure using viscous flow codes suggest that the blades sections should yield efficient performance, characteristic of controlled diffusion aerofoils being introduced in modern gas turbines. Design for stators using the method for validations studies in NAL experimental compressor facility and for a contemporary design are suggested.

Item Type: Monograph (Project Report)
Uncontrolled Keywords: Controlled diffusion aerofoils, transonic compressors
Subjects: AERONAUTICS > Aircraft Propulsion and Power
Depositing User: Ms Indrani V
Date Deposited: 19 Dec 2012 04:21
Last Modified: 25 Jun 2013 08:02
URI: http://nal-ir.nal.res.in/id/eprint/11401

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