Development of Aircraft Sandwich Parts
Abstract
The presented paper shows the design and development process of sandwich parts. A spoiler plate and a main landing gear door are developed. Sandwich parts are made of C/E composite facings and a foam core. FE models have been used for optimization of structures. Emphasis has been placed on deformations of parts under a few load cases. Experimental tests have been used for a verification of structure parts loaded by concentrated forces.Downloads
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Published
2000-01-04
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Copyright (c) 2015 Acta Polytechnica
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