正文
《结构与土木工程前沿(英文)》 >> 2019年 第13卷 第3期 doi: 10.1007/s11709-018-0493-3
Impact analysis of compressor rotor blades of an aircraft engine
. Department of Aeronautical Engineering, Institute of Aeronautical Engineering, Dundigal, Hyderabad 500043, India.. Department of Aeronautical Engineering, College of Engineering, Defense University, Bishoftu 1041, Ethiopia.. School of Mechanical Sciences, Indian Institute of Technology Bhubaneswar, Bhubaneswar 752050, India
摘要
关键词
axial flow compressor ; rotor and stator blades ; aircraft engine ; stress and impact analysis ; aluminum alloys
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