Information Technology and Computer Application Engineering – Liu, Sung & Yao (Eds)
© 2014 Taylor & Francis Group, London, ISBN 978-1-138-00079-7
Finite element analysis of aircraft skin clamping deformation
based on the technology of vacuum adsorption
Da Wei Wu, Hong Min Cui, Ying Chun Liu & Wei Ji
Key Laboratory of Fundamental Science for National Defense of Aeronautical Digital Manufacturing Process,
Shenyang Aerospace University, Shenyang, China
ABSTRACT: As the aircraft skin is less rigid and it requires a higher degree on the surface roughness of the
aircraft skin, therefore it can easily have the problem of clamping deformation in the process of assembly. In
this paper, the aluminum alloy of aircraft skin is regarded as a typical example,