Zobrazeno 1 - 10
of 236
pro vyhledávání: '"Aeroelastic tailoring"'
Autor:
Ahsan Ayaz, Iqbal Rasool Memon, Fahad Ali, Sheharyar Malik, Umer Hameed Shah, Usman Ghafoor, Muhammad Umer, Usama Waleed Qazi
Publikováno v:
IEEE Access, Vol 12, Pp 106042-106055 (2024)
Top speed of an aircraft is limited by the stiffness and damping of a structure which are contributing to aeroelastic response such as divergence and flutter, respectively. This study explores stiffness tailoring of Carbon Fiber Reinforced Polymer (C
Externí odkaz:
https://doaj.org/article/0371d9d647e14df3b120abe711321f87
Autor:
Najmi, Junaid a, ∗, Khan, Haris Ali a, Javaid, Syed Saad a, Hameed, Asad a, Siddiqui, Faisal b
Publikováno v:
In Heliyon 30 January 2024 10(2)
Publikováno v:
Heliyon, Vol 10, Iss 2, Pp e24151- (2024)
This study presents a brief account of the seminal works on aeroelastic tailoring for aerospace applications. Tailoring using advanced composites is a revolutionary process in the ever-evolving realm of aerospace design. The rapid growth in scientifi
Externí odkaz:
https://doaj.org/article/bdc39b4140f545b6bf770b6123d22b9d
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:
Journal of Engineering, Vol 18, Iss 08 (2023)
The paper presents an investigation to the flutter speed of composite wing for different ply orientation. Structurally the composite wing was idealized as a composite beam load carrying structure. Theodorsen’s expression was used to get the 2- dime
Externí odkaz:
https://doaj.org/article/97e8b386cdaf45a1a4bbbbc11e8d1269
Autor:
Kobelev, Vladimir
Publikováno v:
Multidiscipline Modeling in Materials and Structures, 2018, Vol. 15, Issue 2, pp. 365-386.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/MMMS-02-2018-0019
Autor:
Wolf R. Krüger, Yasser M. Meddaikar, Johannes K. S. Dillinger, Jurij Sodja, Roeland De Breuker
Publikováno v:
Aerospace, Vol 9, Iss 10, p 535 (2022)
This article presents the application of aeroelastic tailoring in the design of wings for a flying demonstrator, as well as the validation of the design methodology with flight test results. The investigations were performed in the FLEXOP project (Fl
Externí odkaz:
https://doaj.org/article/5a019dc5ae0645d1a500ff5090b64a0f
Autor:
Aniello Daniele Marano, Marika Belardo, Jacopo Beretta, Filomena Starace, Salvatore Orlando, Claudio Punzi, Raffaele Frajese, Nicola Paletta, Luigi Di Palma
Publikováno v:
Aerospace, Vol 9, Iss 7, p 335 (2022)
The tiltrotor wing structure is one of the most critical and heavily investigated structures in design due to the fundamental need to consider the interactions between the wing, pylon, and rotor systems to achieve aircraft aeroelastic stability. Inde
Externí odkaz:
https://doaj.org/article/d0ff793b3f3f41c1b24b302030bc839f
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