Foam core impresses in aircraft study

2014 ◽  
Vol 58 (6) ◽  
pp. 31-33 ◽  
Keyword(s):  
2002 ◽  
Author(s):  
John J. Young Jr
Keyword(s):  

PAMM ◽  
2021 ◽  
Vol 20 (1) ◽  
Author(s):  
Ahmad Y. Al-Maharma ◽  
Polat Sendur ◽  
Sandeep P. Patil ◽  
Bernd Markert

Composites ◽  
1993 ◽  
Vol 24 (5) ◽  
pp. 447-450 ◽  
Author(s):  
C. Hiel ◽  
D. Dittman ◽  
O. Ishai

Materials ◽  
2020 ◽  
Vol 14 (1) ◽  
pp. 12
Author(s):  
Łukasz Święch ◽  
Radosław Kołodziejczyk ◽  
Natalia Stącel

The work concerns the experimental analysis of the process of destruction of sandwich structures as a result of circumferential shearing. The aim of the research was to determine the differences that occur in the destruction mechanism of such structures depending on the thickness and material of the core used. Specimens with a Rohacell foam core and a honeycomb core were made for the purposes of the research. The specimen destruction process was carried out in a static loading test with the use of a system introducing circumferential shear stress. The analysis of the tests results was made based on the load-displacement curves, the maximum load, and the energy absorbed by individual specimens. The tests indicated significant differences in the destruction mechanism of specimens with varied core material. The specimen with the honeycomb core was characterized by greater stiffness, which caused the damage to occur locally in the area subjected to the pressure of the punch. In specimens with the foam core, due to the lower stiffness of that core, the skins of the structure were bent, which additionally transfers compressive and tensile loads. This led to a higher maximum force that the specimens obtained at the time of destruction and greater energy absorption.


2007 ◽  
Vol 45 (4) ◽  
pp. 432-438 ◽  
Author(s):  
E. Magnucka-Blandzi ◽  
K. Magnucki

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