Zobrazeno 1 - 10 of 21 pro vyhledávání: '"Saiaf Bin Rayhan"'
1
Akademický článek
Crashworthiness Study of a Newly Developed Civil Aircraft Fuselage Section with Auxiliary Fuel Tank Reinforced with Composite Foam
Autor: Saiaf Bin Rayhan, Xue Pu
Publikováno v: Aerospace, Vol 10, Iss 3, p 314 (2023)
Over the past two decades, aircraft crashworthiness has seen major developments, mainly with modern computing systems and commercial finite element (FE) codes. The structure and the material have been designed to absorb more kinetic energy to ensure
Externí odkaz: https://doaj.org/article/ca7d844aaeb64fcd90c3fcdb636129ce
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2
Akademický článek
Dynamic Response of Structurally Reinforced Wing Leading Edge against Soft Impact
Autor: Muhammad Azeem Aslam, Saiaf Bin Rayhan, Ke Zhang
Publikováno v: Aerospace, Vol 9, Iss 5, p 260 (2022)
In this current research, a commercial aircraft metallic leading edge structurally reinforced with a Y-shaped and V-shaped plate system is numerically examined to investigate the effectiveness of such reinforcements against soft impacts, more commonl
Externí odkaz: https://doaj.org/article/d25e94dc321a4fd29cc51de5d4249ccf
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3
Design of an Unmanned Aerial Vehicle for Emergency Situations
Autor: Nafiz Ahmed Khan, Nusrat Jahan, Saiaf Bin Rayhan, Md. Abdus Salam
Current research deals with the design, constructions, and prospective applications of a radio-controlled Unmanned Aerial Vehicle (UAV) which was manufactured for the TÜBİTAK UAV TURKEY competition. The motivation behind this research was for possi
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::5631c026505ba7dbf0c172dbbbdb1778
https://doi.org/10.21203/rs.3.rs-1959462/v1
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4
Effect of micromechanical properties on the critical buckling load of woven composite plate: A multiscale analysis
Autor: Mazedur Rahman, Saiaf Bin Rayhan
Publikováno v: Procedia Structural Integrity. 28:1901-1908
Thin plate buckling is a common failure criterion in aerospace structures that occurs before the material reaches the yield limit (for metal alloys) or the first ply fails (for composites). In general, composites are widely adopted over metallic part
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::d2268e119767322b9f2f3d8a5f57cbda
https://doi.org/10.1016/j.prostr.2020.11.013
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5
Modeling elastic properties of unidirectional composite materials using Ansys Material Designer
Autor: Mazedur Rahman, Saiaf Bin Rayhan
Publikováno v: Procedia Structural Integrity. 28:1892-1900
Advanced reinforced composites are leading materials used in high tech industries (automotive, aerospace, naval, etc.) in recent years. Before manufacturing any structure made by composite materials, it is crucial to analyze their elastic properties
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::e9e09710c3bebed40dcbe02298a7f688
https://doi.org/10.1016/j.prostr.2020.11.012
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8
A Case Study on the Effect of Uncertain Impacts of a Civil Aircraft Fuselage Section With Auxiliary Fuel Tank
Autor: Saiaf Bin Rayhan, Xue Pu
Publikováno v: Volume 4: Advances in Aerospace Technology.
Crashworthiness studies the safety qualification of a vehicle (both airborne and road transports) to protect its occupants during an impact. For an aircraft, specific crashworthiness criteria like deformation pattern of the structure, absorbed kineti
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::c695c064a22726c7fdf4b703ce2e67ed
https://doi.org/10.1115/imece2021-71009
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9
Impact of Micromechanical and Carbon Fiber Properties on the Elastic Modulus of CFRP Woven Composites
Autor: Saiaf Bin Rayhan, Md. Mazedur Rahman
Publikováno v: Proceedings of MEACM 2020 ISBN: 9783030679576
In recent times, Carbon fiber reinforced polymers (CFRP) are widely adopted in various industries such as automobile, aerospace, marine, infrastructure, etc. due to their excellent strength to weight ratio. On the other hand, woven textile composites
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::2ffde221f78a5aeb94f1e3ceb5e680df
https://doi.org/10.1007/978-3-030-67958-3_32
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10
Ballistic gelatin Lagrange Mooney-Rivlin material model as a substitute of bird in finite element bird strike case studies
Autor: Zhange ke, Wang Jing Yu, Muhammad Azeem Aslam, Saiaf Bin Rayhan
Publikováno v: Latin American Journal of Solids and Structures, Volume: 17, Issue: 6, Article number: e298, Published: 18 SEP 2020
Latin American Journal of Solids and Structures v.17 n.6 2020
Latin American journal of solids and structures
Associação Brasileira de Engenharia e Ciências Mecânicas (ABCM)
instacron:ABCM
Numerical simulation plays a crucial role in today’s aviation industry. Modern computers with the latest commercial FE codes have fueled the triumph of establishing simulation as a prerequisite of aerostructure part design from micro modeling of ma
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::380a772faf32d6171bf02705a9777ff5
http://www.scielo.br/scielo.php?script=sci_arttext&pid=S1679-78252020000600508&lng=en&tlng=en
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