Figs.2,4,5 N.A.3.A. Technical keuorun.lum Ho. 914 Figure Oscillorra-n with pressure iistribution in cylinder and marking of arrival of flame at the test point. 0°abs 0°0 5C0 1000 1500 .2000 2500 Figure 4.- Time lapse of combustion process (HSgel)* … Figure 5.- Linear (s 1) ani &£ linear and displacement built up flame propagation (s).
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
