Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Gunasilan Manar"'
Autor:
A. B. M. Supian, M. R. M. Asyraf, Agusril Syamsir, M. I. Najeeb, Abdulrahman Alhayek, Rayeh Nasr Al-Dala’ien, Gunasilan Manar, A. Atiqah
Publikováno v:
Polymers, Vol 16, Iss 11, p 1545 (2024)
Reversible thermochromic polymers have emerged as compelling candidates in recent years, captivating attention for their application in heat detection systems. This comprehensive review navigates through the multifaceted landscape, intricately explor
Externí odkaz:
https://doaj.org/article/7fa3d7e137ec4c549381427e53775e86
Publikováno v:
Advances in Mechanical Engineering, Vol 5 (2013)
Rolled homogeneous armor (RHA) plate subjected to blast loading is a complex problem involving the nonlinear fluid-structure interaction. The numerical techniques using the spatial discretization scheme that has been provided as a solver in the AUTOD
Externí odkaz:
https://doaj.org/article/596366044e3c4150b5067a7a6420e07d
Autor:
Patrice Longère, Gunasilan Manar
Publikováno v:
Engineering Failure Analysis
Engineering Failure Analysis, 2019, ⟨10.1016/j.engfailanal.2019.06.075⟩
Engineering Failure Analysis, Elsevier, 2019, ⟨10.1016/j.engfailanal.2019.06.075⟩
Engineering Failure Analysis, 2019, ⟨10.1016/j.engfailanal.2019.06.075⟩
Engineering Failure Analysis, Elsevier, 2019, ⟨10.1016/j.engfailanal.2019.06.075⟩
This paper presents the experimental investigation of the crack arrest capability under impact loading of two types of aluminum alloys that are mainly used in the field of aeronautics, viz. AA2024 and AA7175. Using gas launcher, impact tests were car
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c79d14e5674ad4893b60bf392b8a1ab9
https://hal.science/hal-02164321/file/S1350630718310744.pdf
https://hal.science/hal-02164321/file/S1350630718310744.pdf
Autor:
Gunasilan, Manar
Les structures aéronautiques peuvent être soumises à des sollicitations sévères telles que les collisions, les impacts de volatiles, etc … Sous l’effet de ces sollicitations rapides, qui du fait de leurs temps caractéristiques très courts
Externí odkaz:
http://www.theses.fr/2018ESAE0027/document
Publikováno v:
DYMAT, 12th International Conference on Mechanical and Physical Behaviour of Materials under Dynamic Loading
DYMAT, 12th International Conference on Mechanical and Physical Behaviour of Materials under Dynamic Loading, Sep 2018, Arcachon, France. pp.02002, ⟨10.1051/epjconf/201818302002⟩
EPJ Web of Conferences, Vol 183, p 02002 (2018)
DYMAT, 12th International Conference on Mechanical and Physical Behaviour of Materials under Dynamic Loading, Sep 2018, Arcachon, France. pp.02002, ⟨10.1051/epjconf/201818302002⟩
EPJ Web of Conferences, Vol 183, p 02002 (2018)
We are here interested in the crack arrest capability under impact loading of metals and polymers used as structural and/or protection materials in aerospace engineering. Kalthoff and Winkler-type impact tests are carried out to that purpose on high
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::516fe541216333cb4ba5dd6d314b4626
https://hal.archives-ouvertes.fr/hal-02151889
https://hal.archives-ouvertes.fr/hal-02151889
Autor:
Gunasilan Manar, Patrice Longère
Publikováno v:
ICEAF V-5th International Conference of Engineering Against Failure-Proceeding
ICEAF V-5th International Conference of Engineering Against Failure-Proceeding, Jun 2018, Chios Island, Greece
MATEC Web of Conferences, Vol 188, p 02005 (2018)
ICEAF V-5th International Conference of Engineering Against Failure-Proceeding, Jun 2018, Chios Island, Greece
MATEC Web of Conferences, Vol 188, p 02005 (2018)
In the context of the design of aeronautical structures regarding accidental events, we are here investigating and comparing the shear failure of two aluminum alloys, namely AA2024 and AA7175, under high strain rate loading. With this aim in view, tw
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7dd15ac0fc6d1b967e2d68859b5ddad2
https://hal.science/hal-01822366
https://hal.science/hal-01822366
Autor:
Md. Fuad Shah Koslan, Ahmad Zaidi Ahmad Mujahid, Gunasilan Manar, Shohaimi Abdullah, Mohd Salleh Bin Mohd Tahir
Publikováno v:
Applied Mechanics and Materials. 471:267-272
The majority of aircrafts structure cracks due to fatigue are thin gage metallic structures and secondary support structures. Beside lower fatigue strength, they may also occur due to mechanical defects, especially at weak area and for areas exposed