Development of Aircraft Sandwich Parts
AbstractThe 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.
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How to Cite
Křena, J., & Cabrnoch, B. (2000). Development of Aircraft Sandwich Parts. Acta Polytechnica, 40(4). Retrieved from https://ojs.cvut.cz/ojs/index.php/ap/article/view/126
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