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ZENODO
Article . 2017
License: CC BY
Data sources: Datacite
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ZENODO
Article . 2017
License: CC BY
Data sources: ZENODO
Claim

Design And Analysis Of Wing Of An Ultralight Aircraft

descriptionPublicationkeyboard_double_arrow_right Article 30 Apr 2017Publisher:Zenodo
Authors: Sarath Raj N. S*, Chithirai Pon Selvan M, Michael G. Bseliss;

doi: 10.5281/zenodo.569965

Design And Analysis Of Wing Of An Ultralight Aircraft

Abstract

This paper deals with the structural design and analysis of high wing of an ultralight aircraft. The wing design involves its initial considerations like planform selection, location to the aircraft and the structural design involves the design calculations for the selection of airfoil, area of the wing, wing loading characteristics and weight of the wing. The design is done corresponding to the calculated values with the help of designing software ANSYS FLUENT.

Keywords

Ultralight Aircraft, Wing Design, Analysis, CFD, Ansys, Lift, Drag

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popularity
This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.
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influence
This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).
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impulse
This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.
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