A two-viable parameter membrane model for wrinkling analysis of membrane structures

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 4, Issue , 2002, Pages 2108-2115

  Ding, H ^a   Yang, B ^a   Lou, M ^a   Fang, H ^a  

^a University of Southern California ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BOUNDARY CONDITIONS; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; STRESS ANALYSIS;

MEMBRANE STRUCTURES; WRINKLING ANALYSIS;

INFLATABLE STRUCTURES;

EID: 0036079274     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-1460     Document Type: Conference Paper

References (9)

1. Analytical characterization of space inflatable structures - An overview
2. Static and dynamic analysis of partially wrinkled membrane structures
3. Finite element analysis of wrinkling membrane
4. Nonlinear dynamic response of membranes: State of the art
5. Finite element analysis of wrinkling membrane
6. A geometrically nonlinear finite element analysis of wrinkled membrane surfaces by a no-compression
7. Nonlinear analysis of tension structures
8. A new look at smoothing newton methods for nonlinear complementarity problems and box constrained variational inequalities
9. A new approach to wrinkling prediction of space membrane structures