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Impact analysis of compressor rotor blades of an aircraft engine 被引量:1
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作者 Y B SUDHIr SASTrY B G KIrOS +1 位作者 F HAILU r budarapu 《Frontiers of Structural and Civil Engineering》 SCIE EI CSCD 2019年第3期505-514,共10页
Frequent failures due to foreign particle impacts are observed in compressor blades of the interceptor fighter MIG-23 aircraft engines in the Ethiopian air force,supplied by the Dejen Aviation Industry.In this paper,w... Frequent failures due to foreign particle impacts are observed in compressor blades of the interceptor fighter MIG-23 aircraft engines in the Ethiopian air force,supplied by the Dejen Aviation Industry.In this paper,we made an attempt to identify the causes of failure and hence recommend the suitable materials to withstand the foreign particle impacts.Modal and stress analysis of one of the recently failed MIG-23 gas turbine compressor blades made up of the following Aluminum based alloys:6061-T6,7075-T6,and 2024-T4,has been performed,apart from the impact analysis of the rotor blades hit by a granite stone.The numerical results are correlated to the practical observations.Based on the modal,stress and impact analysis and the material properties of the three considered alloys,alloy 7075-T6 has been recommended as the blade material. 展开更多
关键词 AXIAL flow COMPRESSOR ROTOR and STATOR BLADES aircraft engine stress and impact analysis aluminum ALLOYS
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