Geometry scaling technique and application to aerodynamic redesign of multi-stage transonic axial-flow compressors
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference39 articles.
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2. Aerodynamic design and testing of an axial flow compressor with pressure ratio of 23.3:1 for the LM2500+ gas turbine;Wadia;J. Turbomach.,2002
3. Effects of nonuniform blade spacing on compressor rotor forced response and aeroacoustics;Leng;J. Propuls. Power,2020
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