Inside Out Library · Explore
Influence of Combustion-chamber Length on Afterburner Performance (1954)
NASA Technical Reports Server (NTRS) · leaf 21
Combustion-chamber length, L, ft (d) Total-pressure loss parameters. Figure 5. - Concluded. Effect of combustion-chamber length on afterburner performance for several equivalance ratios. Flight Mach number, 1.0; altitude, 35,000 feet; afterburner-inlet pressure, 1600 pounds per square foot absolute.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from Influence of Combustion-chamber Length on Afterburner Performance
More like this
