Zobrazeno 1 - 10
of 44
pro vyhledávání: '"Melin Sahin"'
Autor:
Touraj Farsadi, Majid Ahmadi, Melin Sahin, Hamed Haddad Khodaparast, Altan Kayran, Michael I. Friswell
Publikováno v:
Aerospace, Vol 11, Iss 3, p 193 (2024)
In the field of aerospace engineering, the design and manufacturing of high aspect ratio composite wings has become a focal point of innovation and efficiency. These long, slender wings, constructed with advanced materials such as carbon fiber and em
Externí odkaz:
https://doaj.org/article/bddda7b95b3b4b76a4a958cd65afde8e
Publikováno v:
Aircraft Engineering and Aerospace Technology. 92:355-367
Purpose Structural health monitoring (SHM) has become an attractive subject in aerospace engineering field considering the opportunity to avoid catastrophic failures by detecting damage in advance and to reduce maintenance costs. Fibre Bragg Grating
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::edfaf97c1d69d509d196b6b38f25cc90
https://doi.org/10.1108/aeat-11-2017-0255
https://doi.org/10.1108/aeat-11-2017-0255
Publikováno v:
Key Engineering Materials. 744:332-336
Fibre Bragg Grating (FBG) sensors are frequently being used for Structural Health Monitoring (SHM) of aerospace structures. One of the most important advantages of using FBG sensors is that it is possible to embed them into composites. In this paper,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fc7ed7c8f264552d44dfd5499973bc95
https://doi.org/10.4028/www.scientific.net/kem.744.332
https://doi.org/10.4028/www.scientific.net/kem.744.332
Autor:
Ahmet Levent Avsar, Melin Sahin
Publikováno v:
Smart Structures and Systems. 18:249-265
A bimorph piezoelectric energy harvester is developed for harvesting energy under the vortex induced vibration and it is integrated to a host structure of a trapezoidal plate without changing its passive dynamic properties. It is aimed to select trap
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::428813cb03deec8ecebb22fc25192152
https://doi.org/10.12989/sss.2016.18.2.249
https://doi.org/10.12989/sss.2016.18.2.249
Autor:
Serkan Özgen, İlhan Ozan Tunçöz, Melin Sahin, Pınar Arslan, Uğur Kalkan, Yosheph Yang, Yavuz Yaman, Ercan Gürses, Harun Tıraş
Publikováno v:
Journal of Intelligent Material Systems and Structures. 28:979-991
In this article, the design and analysis of a hybrid trailing edge control surface of an unmanned aerial vehicle are presented. The structural design was performed to increase and decrease the camber of the control surface to match selected airfoil p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cea5c78ba453f322302ddab38f01d50a
https://doi.org/10.1177/1045389x16641200
https://doi.org/10.1177/1045389x16641200
Publikováno v:
Structural Health Monitoring, Photogrammetry & DIC, Volume 6 ISBN: 9783319744759
Mechanical amplifiers are employed to enhance output displacement of piezoelectric actuators. Dynamic behavior of such an amplified piezoelectric actuator needs to be known accurately in order to verify its suitability for the driven system. The obje
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9118d6416ca7379d7a204363c2d8ec3f
https://doi.org/10.1007/978-3-319-74476-6_11
https://doi.org/10.1007/978-3-319-74476-6_11
Autor:
Pınar Arslan, Uğur Kalkan, İlhan Ozan Tunçöz, Yavuz Yaman, Serkan Özgen, Ercan Gürses, Harun Tıraş, Melin Sahin, Yosheph Yang
Publikováno v:
Aerospace, Vol 2, Iss 3, Pp 482-504 (2015)
Aerospace
Volume 2
Issue 3
Pages 482-504
Aerospace
Volume 2
Issue 3
Pages 482-504
The idea of morphing is drawing extensive attention in aerospace technologies. Several different approaches like span, camber, twist, and sweep are finding applications. In this work, the concept of a trailing edge control surface which is capable of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::30f5c5aeb2dca216581d1c2011e2c01e
http://www.mdpi.com/2226-4310/2/3/482
http://www.mdpi.com/2226-4310/2/3/482
Due the fact that aircraft structures work in an environment with lots of dynamic forces, it is of vital importance to perform a dynamic analysis to understand dynamic characteristics of aircraft in that specific environment. These characteristics ar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b5a5bd1cefa613aa71e507c9ed878ee1
http://hdl.handle.net/20.500.11851/1530
http://hdl.handle.net/20.500.11851/1530
Autor:
Ahmet Levent Avsar, Melin Sahin
Publikováno v:
25th AIAA/AHS Adaptive Structures Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1b604f414d4cdef1a0b8815561b718a1
https://doi.org/10.2514/6.2017-0729
https://doi.org/10.2514/6.2017-0729
Autor:
Yunus Aksoy, Melin Sahin
Publikováno v:
Insights and Innovations in Structural Engineering, Mechanics and Computation
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::70536efd9f04a958e2f274a430380bcc
https://doi.org/10.1201/9781315641645-15
https://doi.org/10.1201/9781315641645-15