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Influence of Combustion-chamber Length on Afterburner Performance (1954)
NASA Technical Reports Server (NTRS) · leaf 24
MCA EM E54E06 24 Figure 7. - Effect of combustion-chamber length on altitude operational limit. Flight Mach number, 0.8. … Figure 8. - Effect of combustion-chamber length on lean combus- tion blow-out operational limits.NASA Technical Reports Server (NTRS)
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