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...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Departamento de Ciência e Tecnologia Aeroespacial
2020-03-01
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| Series: | Journal of Aerospace Technology and Management |
| Subjects: | |
| Online Access: | http://www.scielo.br/pdf/jatm/v12/2175-9146-jatm-12-e0720.pdf |