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Research Paper

Year: 2018 | Month: October | Volume: 5 | Issue: 10 | Pages: 250-260

Articulation & Analysis of Span Adaptive Wing Using Wind Tunnel<

Summaiya Fatima¹, Mohammad Adnan²

¹Department of Aeronautics, Mahaveer Institute of Science & Technology, Hyderabad
²Jawaharlal Nehru Technological University-Hyderabad, Telengana, India.

Corresponding Author: Summaiya Fatima

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.

Key words: span adaptive wing, wind tunnel, aerodynamic, stability.

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