Investigation on low velocity impact behavior of sandwich composite and monolithic laminate plates using FEM analysis

2019 ◽  
Vol 220 ◽  
pp. 842-846 ◽  
Author(s):  
Hyunbum Park
2014 ◽  
Vol 49 (26) ◽  
pp. 3285-3295 ◽  
Author(s):  
Seyyed Ahmad Hosseini ◽  
Mojtaba Sadighi ◽  
Reza Maleki Moghadam

2021 ◽  
Vol 276 ◽  
pp. 114567
Author(s):  
Amirreza Tarafdar ◽  
Gholamhossein Liaghat ◽  
Hamed Ahmadi ◽  
Omid Razmkhah ◽  
Sahand Chitsaz Charandabi ◽  
...  

2015 ◽  
Vol 50 (6) ◽  
pp. 761-770 ◽  
Author(s):  
Hasan Ulus ◽  
Tugay Üstün ◽  
Ömer Sinan Şahin ◽  
Salim Eğemen Karabulut ◽  
Volkan Eskizeybek ◽  
...  

2013 ◽  
Vol 710 ◽  
pp. 136-141
Author(s):  
Li Jun Wei ◽  
Fang Lue Huang ◽  
Hong Peng Li

Sandwich composite laminates structure is a classic application of composite material on actual aircraft structural. Dealing with low-velocity impact damage and residual compressive strength of sandwich composite laminates, explicit finite element method of ABAQUS/Explicit software was adopted to simulate low-velocity impact and compression process. Impact response and invalidation on compression between sandwich composite laminates with different core materials and regular composite laminates were compared. The simulation results indicated that softer core materials can absorb more impact energy, reduce the structure damage and enhance the residual compressive strength after impact.


2018 ◽  
Vol 27 (5) ◽  
pp. 2505-2512 ◽  
Author(s):  
Andrew J. Turner ◽  
Mohammed Al Rifaie ◽  
Ahsan Mian ◽  
Raghavan Srinivasan

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