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Additional info for Aerotech IV: Recent Advances in Aerospace Technologies: Selected, Peer Reviewed Papers from the AEROTECH IV, November 21-22, 2012, Kuala Lumpur, Malaysia

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Mpkhtar, H. Hasini, M. Yusof and M. Idris, Investigations on the effect of blade angle on the ventilated brake disc using CFD, vol. 376 , no. HTD(1), 2005. [2] K. Munisamy, Aerodynamics of car brake disc cooling with improved design via computational fluid dynamics, Bedfordshire: Cranfield University, 2002. [3] R. Limpert, The thermal performance of automotive disc brakes, vol. 750873, 1975. [4] A. Sission, Thermal analysis of vented brake rotors, vol. 780352, 1978. [5] T. Newcomb, Energy dissipated during braking, Proceedings of Wear, pp.

24 AEROTECH IV Although the comparison by no means rigorous, it may shed some light on how the geometrical modeling and the flapping motion considered in the computational modeling may contribute to the total lift produced and how further refinement could be synthesized. Parametric Study A parametric study is carried out to assess the influence of some flapping wing motion parameters to the flight performance desired. The study considers the following parameters: the Effect of Forward speed, the Effect of Flapping Frequency, the Effect of Lag Angle, the Effect of Angle of Incidence and the Effect of Total Flapping Angle.

A. Ahmad 41 surface of the canard was visualized using mini tuft. Results show that the increment of lift caused by the canard surface setting angle is small and drag is higher as the canard angle is increased and decreased. At positive angles of attack, the moment increases when the canard angle is increased, however at δ = 20˚, the moment decreases due to the separation flow at the upper surface of canard. It is recommended that more studies which look at the larger aspect ratio of canard to be done.

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