Failure analysis of J85-CAN-15 turbojet engine compressor disc
Author:
- Tamer SaraçyakupoğluTSTamer Saraçyakupoğlu
- 1 January 2021
- journal article
- research article
- Published by Elsevier in Engineering Failure Analysis
- Vol. 119
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Failure analysis of inlet guide vane (IGV) actuator and bellcrank assembly used on J85 turbojet enginesEngineering Failure Analysis, 2020
- Topical Issues in Aircraft Health Management with Applications to Jet EnginesINCAS BULLETIN, 2020
- Metallurgical Failure Analysis2018
- Study of the current incentive rules and mechanisms to promote biofuel use in the EU and their possible application to the civil aviation sectorTransportation Research Part D: Transport and Environment, 2016
- The Review of Manufacturing Technology for Aircraft Structural PartProcedia CIRP, 2016
- Designation of Environmental Impacts and Damages of Turbojet Engine: A Case Study with GE-J85Atmosphere, 2014
- Investigations on fretting fatigue in aircraft engine compressor bladeEngineering Failure Analysis, 2011
- Effect of three-dimensional loading on macroscopic fretting aspects of an aero-engine blade–disc dovetail interfaceTribology International, 2011
- Failure analysis of J85 Engine turbine bladesEngineering Failure Analysis, 2008
- Gas Turbine Performance2004