Aerotech IV: Recent Advances in Aerospace Technologies: by R. Varatharajoo, E. J. Abdullah, D. L. Majid, F. I. Romli,

By R. Varatharajoo, E. J. Abdullah, D. L. Majid, F. I. Romli, A. S. Mohd Rafie

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Extra resources 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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The FMV was used to solve the continuity, momentum and energy equations with the associated boundary conditions. The two-dimensional double precision version R. Varatharajoo, E. J. Abdullah, D. L. Majid, F. I. Romli, A. S. Mohd Rafie and K. A.

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. The results are exhibited in Fig. 9. Motion Based Forces Splitting Another study is carried out to investigate the influence of individual contributions of the pitching-flapping motion and their phase lag on the flight performance. The calculation is performed on rectangular wing. Results obtained as exhibited in Fig.

The measurement of air core diameter was taken based on that microscale image to get more accurate result. (a) (b) (c) Fig. 3 Sample images of a) Microscale lens inside the atomizer with water, b) Microscale lens and c) Microscale magnification R. Varatharajoo, E. J. Abdullah, D. L. Majid, F. I. Romli, A. S. Mohd Rafie and K. A. Ahmad 35 To ascertain the accuracy of the aircore diameter measurement, test have been carried out with four diffrent wire of known diameter located centrally inside the swirl chamber.

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