Composite, grid-stiffened panel design for post buckling using Hypersizer®

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

Volumn 1, Issue , 2002, Pages 157-172

  Collier, Craig ^a   Yarrington, Phil ^a   Van West, Barry ^a  

^a Collier Research Corporation ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; COMPOSITE STRUCTURES; FAILURE ANALYSIS; HONEYCOMB STRUCTURES; SANDWICH STRUCTURES; STIFFNESS; STRUCTURAL LOADS;

SANDWICH PANELS;

STRUCTURAL PANELS;

EID: 0036075686     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Thermoelastic formulation of stiffened, unsymmetric composite panels for finite element analysis of high speed aircraft
2. The hypersizing method for structures
3. The strength of thin plates in compression
4. Effective widths of compression-loaded plates with a cutout
5. Prebuckling and postbuckling response of tailored composite stiffened panels with axial-shear coupling