Models and tools for heat transfer, thermal stresses, and stability of composite aerospace structures

Journal of Thermal Stresses

Volumn 26, Issue 6, 2003, Pages 641-670

  Rolfes, R ^a   Tessmer J ^a   Rohwer, K ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

Composites; Fiber Metal Laminates; Heat Transfer; Hybrid Structures; Thermal Buckling; Thermal Stresses

Indexed keywords

BOUNDARY CONDITIONS; BUCKLING; COMPOSITE STRUCTURES; FINITE ELEMENT METHOD; HEAT TRANSFER; MATHEMATICAL MODELS; STABILITY; THERMAL STRESS;

COMPOSITE AEROSPACE STRUCTURES; FLAPS; THERMALLY INDUCED BUCKLING;

AIRCRAFT PARTS AND EQUIPMENT;

EID: 0242526873     PISSN: 01495739     EISSN: 1521074X     Source Type: Journal    
DOI: 10.1080/713855951     Document Type: Article

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