Numerical simulation of the transient response of blade due to bird impact

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 24, Issue 6, 2003, Pages 531-533

  Chen, Wei ^a   Guan, Yu Pu ^a   Gao, De Ping ^a  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

Bird impact; Blade; Numerical simulation; Transient response

Indexed keywords

AIRCRAFT ENGINES; COMPUTER SIMULATION; FINITE ELEMENT METHOD;

BIRD IMPACT; NUMERICAL SIMULATION; TRANSIENT RESPONSE;

TURBOMACHINE BLADES;

EID: 1942508178     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (8)

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4. Whirley R G, Engelmann B E. An automatic contact algorithm in Dyna3D for impact problems [R]. UCRL-JC-114820, 1993
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