Foreign object damage to fan rotor blades of aeroengine part II: Numerical simulation of bird impact

Chinese Journal of Aeronautics

Volumn 21, Issue 4, 2008, Pages 328-334

  Guan, Yupu ^a   Zhao, Zhenhua ^a   Chen, Wei ^a   Gao, Deping ^a  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

Aerospace propulsion system; Bird impact; Fan rotor blade; Numerical simulation; Transient response

Indexed keywords

AIRCRAFT ACCIDENTS; AIRCRAFT ENGINES; AIRCRAFT PROPULSION; COMPUTER SIMULATION; NUMERICAL MODELS; PROPULSION; TRANSIENT ANALYSIS; TURBOMACHINE BLADES;

AEROSPACE PROPULSION SYSTEM; AIRCRAFT COMPONENTS; BIRD IMPACT; COMPUTATIONAL MODEL; EQUIVALENT STRESS; FAN ROTOR BLADES; FOREIGN-OBJECT DAMAGE; MAXIMUM DISPLACEMENT;

BIRDS;

EID: 50849086052     PISSN: 10009361     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1000-9361(08)60043-6     Document Type: Article

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