Study of Design Modification Effects through Performance Analysis of a Legacy Gas Turbine Engine

Study of Design Modification Effects through Performance Analysis of a Legacy Gas Turbine Engine

Modifications to the critical parameters, such as the exhaust nozzle area, are sometimes done during maintenance of aircraft engines. These modifications are done either to increase the design thrust or to compensate for the reduction of thrust due to leakage in the variable area jet nozzle. There...

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Bibliographic Details
Main Authors:	Gantayata Gouda, Balaji Sankar, Venkat Iyengar, Jana Soumendu
Format:	Article
Language:	English
Published:	Departamento de Ciência e Tecnologia Aeroespacial 2020-03-01
Series:	Journal of Aerospace Technology and Management
Subjects:	aerothermodynamic model twin spool turbojet engine multipoint map scaling compressor characteristics map
Online Access:	http://www.scielo.br/pdf/jatm/v12/2175-9146-jatm-12-e0720.pdf

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