Turbine And Compressor Design: A Comprehensive Study Of Gas Turbine Components, Cooling Techniques, Aerodynamic Instabilities, And Axial Compressor Design
Author : Mrs.J.Jaisy Journa Name: International Journal of Scientific Research & Engineering Trends Volume: 12 issue: 3 Year: Volume-12-issue-3 Views : 88Gas turbines are among the most important energy conversion systems used in aerospace propulsion, power generation, and industrial applications. This paper presents a comprehensive review of turbine and compressor design principles, thermodynamic operation, cooling technologies, aerodynamic instabilities, and axial compressor design methodologies. Particular emphasis is placed on compressor staging, velocity-triangle analysis, turbine cooling methods, stall mechanisms, and surge phenomena. The paper synthesizes fundamental design approaches and provides a structured framework suitable for engineering education and preliminary turbomachinery design studies.
Related Indexing Platform
Indexed Journal Website
OAI
https://abcdindex.com/Q745YUJGHTHWE77/ajax/paper_indexing_from_deng.php?verb=GetRecord&identifier=oai%3Aabcdindex.com%3Aarticle%3A65765&metadataPrefix=oai_dc
ABCDIndex OAI-PMH
Dublin Core metadata (harvesters)
GS
Search on Google Scholar
Google Scholar
Search this title on Scholar
SS
Search on Semantic Scholar
Semantic Scholar
Search this title