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- W2010109344 abstract "test conditions, the agreement with the theoretical data was fair. The results may be found in Ref. 1. To verify the influence of Mach number, the data for cone air injection data according to Pappas and Okuno were used at a cone Mach number Mc = 4.35. The result is shown in Fig. 2 where the cooling effectiveness 77 = l/(K + 1) has been given as a function of the blowing ratio F. A Prandtl number of 0.75 was used. The experimental curve represents the data at x = 8.19 in. For comparison, the curve at M = 0 has also been included in Fig. 2. It is seen that the actual Mach number theoretical results indicate reasonable agreement with the test data and represent significant improvement over the zero Mach number approach." @default.
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- W2010109344 date "1968-08-01" @default.
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- W2010109344 title "Plane and spherical detonation waves in solid explosives." @default.
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- W2010109344 doi "https://doi.org/10.2514/3.4829" @default.
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