Turbojet thrust augmentation by evaporation of water prior to mechanical compression as determined by use of psychrometric chart

E. Clinton Wilcox
naca-tn-2105
Jun 1950

The thrust augmentation of a turbojet engine resulting from the evaporation of water prior to mechanical compression was investigated over a range of flight Mach numbers, altitudes, ambient temperatures, and ambient relative humidities.

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http://naca.central.cranfield.ac.uk/reports/1950/naca-tn-2105.pdf