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Clarification about Component Mode Synthesis Methods for Substructures with Physical Flexible Interfaces
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  • Clarification about Component Mode Synthesis Methods for Substructures with Physical Flexible Interfaces
  • Clarification about Component Mode Synthesis Methods for Substructures with Physical Flexible Interfaces
저자명
Ohayon. R.,Soize. C.
간행물명
International journal of aeronautical and space sciences
권/호정보
2014년|15권 2호|pp.113-122 (10 pages)
발행정보
한국항공우주학회
파일정보
정기간행물|ENG|
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이 논문은 한국과학기술정보연구원과 논문 연계를 통해 무료로 제공되는 원문입니다.
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기타언어초록

The objective of the paper is to clarify a methodology based on the use of the existing component mode synthesis methods for the case of two damped substructures which are coupled through a linking viscoelastic flexible substructure and for which the structural modes with free geometrical interface are used for each main substructure. The proposed methodology corresponds to a convenient alternative to the direct use either of the Craig-Bampton method applied to the three substructures (using the fixed geometric interface modes) or of the flexibility residual approaches initiated by MacNeal (using the free geometric interface modes). In opposite to a geometrical interface which is a topological interface on which there is a direct linkage between the degrees of freedom of substructures, we consider a physical flexible interface which exists in certain present technologies and for which the general framework linear viscoelasticity is used and yields a frequency-dependent damping and stiffness matrices of the physical flexible interface.