Zobrazeno 1 - 10
of 33
pro vyhledávání: '"Touraj Farsadi"'
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:
Acta Mechanica. 233:3233-3252
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::163c565890e38ad94b0f753ef414da74
https://doi.org/10.1007/s00707-022-03238-y
https://doi.org/10.1007/s00707-022-03238-y
Publikováno v:
International Journal of Aeronautical and Space Sciences.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4424e83548fe42ef14134ae818eb47c4
https://doi.org/10.1007/s42405-023-00603-6
https://doi.org/10.1007/s42405-023-00603-6
Publikováno v:
AIAA Journal. 59:1422-1440
In the present study, the flutter performance of a composite thin-walled beam wing–engine system is optimized by implementing two different control approaches: 1) passive open-loop and 2) active cl...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0aab570a78424a86b51fe5d63091bf73
https://doi.org/10.2514/1.j059568
https://doi.org/10.2514/1.j059568
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 235:2017-2032
This study presents the use of variable stiffness concept via curvilinear fiber placement to achieve improved structural characteristics in composite thin-walled beams (TWBs). The TWB used in the study is constructed in circumferentially asymmetric s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e6918522d9ca555c14243694f6a0bbdf
https://doi.org/10.1177/0954410020988240
https://doi.org/10.1177/0954410020988240
Autor:
Hasan Kurtaran, Touraj Farsadi
Publikováno v:
Volume: 4, Issue: 2 36-47
Journal of Aviation
Journal of Aviation
Bu çalışmada, eğrisel fiber kompozit çift eğimli panelin temel doğal frekansları optimize edilmiştir. Hava-uzay araçlarının yapısal çerçevelerinin çeşitli bileşenlerinde çift kıvrımlı paneller kullanılmaktadır. Değişken sert
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c2f00933d68292b1a38e069f36200548
https://doi.org/10.30518/jav.787455
https://doi.org/10.30518/jav.787455
Publikováno v:
Acta Mechanica. 232:555-573
In this study, natural frequencies and vibrational mode shapes of variable stiffness composite skewed plates are optimized applying a genetic algorithm. The variable stiffness behavior is obtained by altering the fiber angles continuously according t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7b450181b9a630fd7ffeba633e4e5c75
https://doi.org/10.1007/s00707-020-02871-9
https://doi.org/10.1007/s00707-020-02871-9
Autor:
Touraj Farsadi, Altan Kayran
Publikováno v:
Wind Energy. 24:69-91
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6ca04318e14df1908e30695a4bb0f7c6
https://doi.org/10.1002/we.2559
https://doi.org/10.1002/we.2559
Autor:
Touraj Farsadi, Davood Asadi
Publikováno v:
Journal of Aviation. 4:1-14
In the present study, the aeroelastic energy response of a twin-engine composite wing system is optimized based on sequential quadratic programming (SQP) method. The variable stiffness is acquired by constructing laminates of thin wall beam (TWB) wit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2db55ab4ef0760e7b38c81374247c5be
https://doi.org/10.30518/jav.668240
https://doi.org/10.30518/jav.668240
Publikováno v:
Acta Mechanica. 231:715-731
In the present study, nonlinear flutter and post-flutter behavior of a variable stiffness composite wing-like plate is investigated. The variable stiffness is obtained by varying fiber angles continuously according to a selected curvilinear fiber pat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1b1897cb4f2308f3467cdc17629b4017
https://doi.org/10.1007/s00707-019-02564-y
https://doi.org/10.1007/s00707-019-02564-y