Thermally induced loads of fastened hybrid composite/aluminum structures

Journal of Aircraft

Volumn 45, Issue 2, 2008, Pages 569-580

  Yang, Chihdar ^a,b   Sun, Wenjun ^a,b   Seneviratne, Waruna ^a,c   Shashidhar, Ananthram K ^a,b  

^a WICHITA STATE UNIVERSITY   (United States)

^b Department of Aerospace Engineering ^*

^c National Institute for Aviation Research

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM; AVIATION; FUSELAGES; THERMAL EXPANSION; THERMAL STRESS;

AIRCRAFT FUSELAGES; ANALYTICAL MODELS; AVIATION INDUSTRIES; HYBRID COMPOSITES;

COMPOSITE STRUCTURES;

EID: 42949123490     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.31776     Document Type: Article

References (9)