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Extra info for Aerotech IV: Recent Advances in Aerospace Technologies: Selected, Peer Reviewed Papers from the AEROTECH IV, November 21-22, 2012, Kuala Lumpur, Malaysia
4. The experimental rig has ability to measure measurements, such as total flow rate, surface temperature and pressure which collected by Data Acquisition System integrated with the test rig. The test rig is measuring the total flow rate using flow meter. A long inlet duct or pipe is fabricated to measure the inlet flow rate after the entrance length where the flow is fully developed region. From the flow rate the average velocity is calculated. The flow rate is used as input to numerical analysis of the computational model.
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. K Som, Initiation of air core in a simplex nozzle and the effects of operating and geometrical parameters on its shape and size, Journal experimental thermal and fluid science.
The area of airflow separation increases as the canard setting angle is increased until the canard is stall completely. The canard is no longer producing lift. As moment is much related to the lift force, this will influence moment coefficient, as observed by its decreasing in Fig. 2(d). As seen in Fig. 2(b) drag decreases as canard setting angles is increased at negative angles of attack. This is due to the fact that at negative angles of attack, the streamline airflow still can be observed at the leading edge and inboard of canard.