Articulation & Analysis of Span Adaptive Wing Using Wind Tunnel

Journal Title: International Journal of Research and Review - Year 2018, Vol 5, Issue 10

Abstract

In this project we will analyse the forces during subsonic flight conditions, the concept of (SAW) span adaptive wing is to fold the outer portion of aircraft wing and there control surfaces to optimal angels in flight. The (SAW) project intends to obtain a wide spectrum of aerodynamic benefits in flight by folding wings. Where it has an ability to fold the outer portion of aircraft wing in flight during subsonic and supersonic manoeuvres, on-board controllers which helps folding of wing panel between the angles of 0-40 deg to bend completely. Hence using span adaptive wing we can attain a superior stability.

Authors and Affiliations

Summaiya Fatima

Keywords

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  • EP ID EP482517
  • DOI -
  • Views 60
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How To Cite

Summaiya Fatima (2018). Articulation & Analysis of Span Adaptive Wing Using Wind Tunnel. International Journal of Research and Review, 5(10), 250-260. https://europub.co.uk/articles/-A-482517