Özet
The purpose of this study is to examine the energy absorption characteristics of nested and concentric crash tubes with different cross sections under low velocity impact loading. They can be used as energy absorbers for the spacecraft vehicle to enhance crashworthiness under impact loads occurring during landing. Numerical analyses are performed by using LS-DYNA and the results are compared and discussed according to peak crash force, absorbed energy, deformations, folding mechanism, SEA and CFE values. As the number of corner is increased at the constant mass, the deformation of the tubes can be limited. Besides better crash force efficiency and lower peak forces are observed in the analyses of less cornered tubes.
Orijinal dil | İngilizce |
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Ana bilgisayar yayını başlığı | Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017 |
Editörler | M.F. Unal, A. Hacioglu, M.S. Yildiz, O. Altan, M. Yorukoglu |
Yayınlayan | Institute of Electrical and Electronics Engineers Inc. |
Sayfalar | 23-27 |
Sayfa sayısı | 5 |
ISBN (Elektronik) | 9781538616031 |
DOI'lar | |
Yayın durumu | Yayınlandı - 4 Ağu 2017 |
Etkinlik | 8th International Conference on Recent Advances in Space Technologies, RAST 2017 - Istanbul, Turkey Süre: 19 Haz 2017 → 22 Haz 2017 |
Yayın serisi
Adı | Proceedings of 8th International Conference on Recent Advances in Space Technologies, RAST 2017 |
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???event.eventtypes.event.conference??? | 8th International Conference on Recent Advances in Space Technologies, RAST 2017 |
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Ülke/Bölge | Turkey |
Şehir | Istanbul |
Periyot | 19/06/17 → 22/06/17 |
Bibliyografik not
Publisher Copyright:© 2017 IEEE.
Finansman
Support for this work has been provided by the Scientific and Technological Research Council of Turkey under Project Number 115M465 and Istanbul Technical University research fund.
Finansörler | Finansör numarası |
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Türkiye Bilimsel ve Teknolojik Araştirma Kurumu | 115M465 |
Istanbul Teknik Üniversitesi |