Journal
AEROSPACE SCIENCE AND TECHNOLOGY
Volume 5, Issue 2, Pages 135-146Publisher
ELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER
DOI: 10.1016/S1270-9638(00)01089-0
Keywords
thermo-mechanics; heat transfer; thermal analysis; thermally induced buckling; structural stability; composites; transport aircraft; wing; fuselage
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Thermo-mechanical design aspects for primary carbon fibre reinforced plastics (CFRP) components, especially wings, of future large transport aircraft are discussed. Numerical simulations of the heating of a wing under intensive sun irradiation and of cooling during taxiing and take-off result in the recommendation of an appropriate design temperature. The study of flat stringer-stiffened panels reveals the influence of imperfections and boundary conditions on the buckling load under simultaneous thermal and mechanical loading. (C) 2001 Editions scientifiques et medicales Elsevier SAS.
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