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Additional info for Aircraft Performance & Design
1. 0 3 4 5 6 7 r (mm) 8 9 1 0 Fig. 6 Radial profiles of the mean temperature, rms fluctuation, and intermittency of the jet fluid at three different heights. •, mean temperature; V, rms fluctuation; 0, Intermittency. Uj = 15 m/s, Ua = 3 m/s. a) z = 5 mm, b) z = 15 mm, c) z = 25 mm.
T. Scarinci would like to thank Dr. David Bull for providing the possibility to clarify the ideas of this paper, while visiting the Thornton Shell Research Center. The work in McGill was supported by NSERC Grants A-7091 and A-3347. T. Scarinci acknowledges the support from an NSERC Postgraduate Scholarship. H. Non-Steady Flame Propagation, AGARDograph no. 75, MacMillian, New York, 1964. , "The Mechanism of Transition from Deflagration to Detonation," Progress in Combustion Science, Vol. 6, 1980, pp.
The intermittency curve expanded outward, and the inner edge of the visible flame zone shifted slightly inward. 2 mm). This finding is again consistent with the photographic observation (Fig. 3b). The interaction between the large-scale vortex and the flame zone became further evident at Uj = 15 m/s (Fig. 5c). 1. 0 3 4 5 6 7 r (mm) 8 9 1 0 Fig. 6 Radial profiles of the mean temperature, rms fluctuation, and intermittency of the jet fluid at three different heights. •, mean temperature; V, rms fluctuation; 0, Intermittency.
Aircraft Performance & Design by Anderson