The knocking characteristics of fuels in relation to maximum permissible performance of aircraft engines (1939)
NASA Technical Reports Server (NTRS) · leaf 10
s shown in reference 11 that the highest in this report. permissible compression ratio without auto-ignition Stansfield and Thole (reference 13) have presented decreased from 9 at a fuel-air ratio of about 0.020 to a the results of tests in which they determined the effect of humidity on the… … 1,300 1,400 1,500 1,600 1,700 1,800 used as the mixture ratio is either increased or decreased Ta, *F. absolute from the approximately chemically correct mixture. Fiocbz 14.—Effect of end-gas temperature on ""fa™ permissible end-gas density In the determination of the curves in figure 14, it was…
NASA Technical Reports Server (NTRS)
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