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
Project No. 600-RMI/ERGS/5/3/ (54/2011). References  Arthur H. Lefebvre, Atomization and sprays, New York: Hemisphere, 1989. A Hamid and R. Atan, Spray characteristics of jet-swirl nozzles for thrust chamber injector, Journal of aerospace science and technology, Vol 13 (2009) 192-196. K Som, A numerical and experimental investigation on the coefficients of discharge and the spray cone angle of a solid cone swirl nozzle, Journal of experimental thermal and fluid science, Vol 28 (2004) 297-305.
Looking at Fig. 6, the velocity vector plot clearly predicts that the air flow concentrates toward the frontal side with more velocity vector at higher velocity region. Another obvious region is along the rear side towards trailing edge of the vane or blade where a major re-circulation and low velocity region predicted. The flow misalignment angle “β” is establish in Fig. 6, which was used as design criteria for curved blade design in this paper. This flow kinematics is inevitable in induce flow pattern inside ventilated channel.
8]. The graph also shows that the air core diameter increases with increasing injection pressure for each atomizer tested. However, at higher range of injection pressure (4 bar and above), the air core diameter has become less dependent on the injection pressure, which is in agreement with the previous research . This is because increasing injection pressure will increase the tangential velocity of injection to the atomizer and increases the strength of swirling motion inside the swirl chamber.
Aerotech IV: Recent Advances in Aerospace Technologies: Selected, Peer Reviewed Papers from the AEROTECH IV, November 21-22, 2012, Kuala Lumpur, Malaysia by R. Varatharajoo, E. J. Abdullah, D. L. Majid, F. I. Romli, A. S. Mohd Rafie