Aerodynamic numeric modelling of a semi rigid hang glider/ultralight wing.

Md.Zain, Zaidi and Mohamad, Nazri and Sapari, Suhaime and Mat Taib, Che Faridah and Ma’som, Nor Azizah (2002) Aerodynamic numeric modelling of a semi rigid hang glider/ultralight wing. In: INSIGHTS Seminar 2002, 24-25 August 2002, Putra World Trade Centre (PWTC).
Abstract

TOP SECRET, a semi-rigid hang glider is currently being designed and built by Lai Mouette S.A., Dijon, France. This paper outlines the aerodynamic design of TOP SECRET. The 2D airfoil was analysed using EPPLER (Prof Richard Eppler, University of Stuttgart) and XFOIL (Prof. Mark Drela, M.I.T.) software. Analysis on the 3D wing was done using Wessinger Extended Lifting Line Theory. The objective was to find the best linear twist angle distribution from root to tip to give the highest Lift/Induced Drag ratio. This is called the Minimum Induced Drag Criteria. The linear distribution was chosen to make construction easy and cheap. Validation using Lifting Surface Theory (Software SURF, Herve Bezard, ONERA) was also done for a “constant chord” and “no twist” wing. The best linear twist is 0° at root and 6° at tip. TOP SECRET was benchmarked against PEGASUS (Germany), a proven semi-rigid hang glider. At the same time, FLUENT computational fluid dynamics software was used to get the polars of the aerofoil for TOP SECRECT and the results was in agreement with the results from EPPLER and SURF.

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