Effect of laminate design and loads on crack opening volume in laminates used in cryogenic tanks

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

Volumn 3, Issue , 2002, Pages 1667-1676

  Noh, Jae ^a   Whitcomb, John ^a  

^a Texas AandM University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT FUEL TANKS; CRACKS; CRYOGENIC EQUIPMENT; DEGRADATION; FINITE ELEMENT METHOD; LEAKAGE (FLUID); LOADS (FORCES); MATHEMATICAL MODELS;

CRYOGENIC TANKS;

LAMINATED COMPOSITES;

EID: 0036077999     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-1415     Document Type: Conference Paper

References (9)

1. Detection of micro-leaks through complex geometries under mechanical load and at cryogenic temperature
2. Modeling of propollent leakage through matrix cracks in composite laminates
3. Effect of various parameters on the effective properties of a cracked ply
4. Analysis of cracked laminates: A variational approach
5. Some new variational mechanics results on composite micro microcracking
6. Analysis of progressive matrix cracking in composite laminates I. Thermoelastic properties of a ply with cracks
7. An analytical model for thermoelastic properties of composites laminates containing transverse matrix cracks