Development of a Methodology to Estimate Aero-Performance and Aero-Operability Limits of a Multistage Axial Flow Compressor for Use in Preliminary Design

Development of a Methodology to Estimate Aero-Performance and Aero-Operability Limits of a Multistage Axial Flow Compressor for Use in Preliminary Design

Bibliographic Details
Main Author: Kulkarni, Sameer
Language:English
Published: Case Western Reserve University School of Graduate Studies / OhioLINK
Subjects:
Aerospace Engineering
Mechanical Engineering
axial compressors
computational fluid dynamics
turbomachinery
Online Access:http://rave.ohiolink.edu/etdc/view?acc_num=case1321453240

Internet

http://rave.ohiolink.edu/etdc/view?acc_num=case1321453240

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