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Akademický článek

Investigation of aerodynamic characteristics of swept C-wing configurations at transonic speed using design of experiments and computational fluid dynamics

Autor: Heershikesh Heerish Samputh, Lip Kean Moey, Vin Cent Tai, Yong Chai Tan

Publikováno v: Aviation, Vol 28, Iss 2 (2024)

Authors investigated the aerodynamic characteristics of backward swept (BSCW) and forward swept (FSCW) C-wing configurations at transonic speed using Design of Experiments (DoE) and Computational Fluid Dynamics (CFD), aiming to enhance aircraft perfo

Externí odkaz: https://doaj.org/article/839f2e82d4ff4686b6d972852e907184

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Akademický článek

Aerodynamic Analysis of C-Wing Aircraft

Autor: R. NAVEEN

Publikováno v: INCAS Bulletin, Vol 10, Iss 3, Pp 157-165 (2018)

In the recent years, the researchers focused on the development of long-range aircraft with the commercial aid of nonconventional design concepts. The C-wing concepts for large aircraft are highly preferred to overcome the design constraints such as

Externí odkaz: https://doaj.org/article/cec4fca19c894eaebb48728dec63b083

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Akademický článek

Study of a C-wing configuration for passive drag and load alleviation

Autor: Skinner, S.N., Zare-Behtash, H.

Publikováno v: In Journal of Fluids and Structures April 2018 78:175-196

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Akademický článek

Aerodynamic Analysis of C-Wing Aircraft.

Autor: NAVEEN, R.¹ aeror.naveen@gmail.com

Publikováno v: INCAS Bulletin. 2018, Vol. 10 Issue 3, p157-165. 9p.

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Akademický článek

Investigation and design of a C-Wing passenger aircraft

Autor: Karan BIKKANNAVAR, Dieter SCHOLZ

Publikováno v: INCAS Bulletin, Vol 8, Iss 2, Pp 25-40 (2016)

A novel nonplanar wing concept called C-Wing is studied and implemented on a commercial aircraft to reduce induced drag which has a significant effect on fuel consumption. A preliminary sizing method which employs an optimization algorithm is utilize

Externí odkaz: https://doaj.org/article/c0f419952026443492d32e97b9585f33

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