Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Raguraman, Munusamy"'
Publikováno v:
Defence Technology, Vol 36, Iss , Pp 71-77 (2024)
Honeycomb sandwich structures are widely used in lightweight applications. Usually, these structures are subjected to extreme loading conditions, leading to potential failures due to delamination and debonding between the face sheet and the honeycomb
Externí odkaz:
https://doaj.org/article/1a931e984984422c949886ffe72076f2
Publikováno v:
International Journal of Crashworthiness. 27:747-758
Composite sandwich panels are commonly considered as lightweight materials for structural design in many applications including automotive, aerospace and defence systems. These panels must be devel...
Publikováno v:
Revue des composites et des matériaux avancés. 30:189-194
Autor:
Wood, Paul, Boud, Fathi, Carter, Wayne, Varasteh, Hirbod, Gunputh, Urvashi, Pawlik, Marzena, Clementson, Jenny, Lu, Yiling, Hossain, Syed, Broderick, Matthew, Raguraman, Munusamy, Smith, Andy, Mantle, Andy, McGourlay, Jamie
Publikováno v:
Journal of Manufacturing & Materials Processing; Dec2022, Vol. 6 Issue 6, p154, 16p
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science. 226:2053-2062
This article deals with the effects of parameters relating to the yield drop phenomenon on the deformation of Taylor projectiles. The numerical modelling approach performed using LS-DYNA was validated by considering a solid cylindrical projectile mad
Autor:
David C. Barton, Raguraman Munusamy
Publikováno v:
International Journal of Crashworthiness. 15:223-234
An important feature of the Formula SAE (Society of Automotive Engineers) race car design competition is that the car must withstand a certain level of frontal impact without intrusion into the driver foot-well area or damaging levels of deceleration
Publikováno v:
DYMAT 2009 - 9th International Conferences on the Mechanical and Physical Behaviour of Materials under Dynamic Loading.
Autor:
David Barton, Raguraman Munusamy
Publikováno v:
International Journal of Aerospace Innovations. 3:i-ii