Effect of position of tension-loaded inserts on honeycomb panels used for space applications

Author:

Slimane S.ORCID,Kebdani S.,Boudjemai A.,Slimane A.

Publisher

Springer Science and Business Media LLC

Subject

Industrial and Manufacturing Engineering,Modeling and Simulation

Reference33 articles.

1. ECSS.: Space Engineering Insert Design Handbook, vol. ECSS-E-HB-32-22A, ed. : ESA-ESTEC, Noordwijk (2011)

2. Zenkert,D.: An introduction to sandwich construction: engineering materials advisory services. Sheffield, UK (1995)

3. Campbell Jr., F.C.: Manufacturing Technology for Aerospace Structural Materials. Elsevier, Amsterdam (2011)

4. D’Amato, E.: Caratterizzazione strutturale di inserti per pannelli in composito, Parte I: Dati Sperimentali, XXXV Convenzione Nazioinale AIAS, Ancona (2006)

5. Thompson, R., Matthews, F., O’Rourke, B.: Load attachment for honeycomb panels in racing cars. Mater. Des. 16, 131–150 (1995)

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