Comparison of Dynamic Behaviour of Structures Subjected to Blast Loads
Citation
Athira Sathyan, A P Beena, Dr. S B Tiwari, Ranjan Abraham"Comparison of Dynamic Behaviour of Structures Subjected to Blast Loads", International Journal of Engineering Trends and Technology (IJETT), V28(9),469-472 October 2015. ISSN:2231-5381. www.ijettjournal.org. published by seventh sense research group
Abstract
An investigation has been carried out to examine
the dynamic behaviour of crew module fairing subjected to
blast loading. The objective of the present study is to
determine the dynamic response of the crew module fairing
with different type of construction such as metallic isogrid and
metallic sandwich subjected to blast load. The crew module
fairing is modelled as a shell structure with rings provided at
different levels with different thickness. The sandwich
structure consists of Aluminium honeycomb core with
Aluminium face skin. The blast load acting on the structure is
applied as a pressure- time curve and it is a triangular pulse
with a rise time of 1 milliseconds and decay time of 6
milliseconds. The dynamic response of the metallic sandwich
and isogrid crew module fairing structure are compared. The
linear dynamic analysis is carried out using the software
ABAQUS.
References
[1] Abdelkrim Kalid “ stiffened plate subjected to uniform blast loading”
journal of civil engineering and management, may 2008 page 155- 161
[2] Goel M. D , Matsagar V. A “ dynamic response of shell structures
subjected to explosive loads” Department of civil engineering (IIT
Delhi), October 1010
[3] Kim Ki C and Joseph C Fries “Dynamic response analysis of GR/EP
composite panels under blast wave pressure loading” AIAA journal ,
April 2005
[4] Murray M.P , Wilson G. and Cloke M . D “ Analytical study of
vehicle structures subjected to a transient blast over pressure” ,AIAA
Jouranl, January 2004
[5] ReinoNiemi, Richard Rabenau "Blast effects on space vehicle
structures" NASA Technical note, NASA TN D-2945, NATIONAL
AERONAUTICS AND SPACE ADMINISTRATION, Washington,
D.C, February 1966
Keywords
Crew Module Fairing, Blast load, Transient
Response Analysis.