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- W1567380891 abstract "Methods are for calculating net thrust using air specific-impulse data for various fuels. Nomographic solutions are given to adapt the methods to turbojet-afterburner calculations. These nomographs can be used to compute net thrusts obtained by expanding exhaust gases to either a Mach number of 1.0 or the ambient static pressure at the nozzle exit. Thermodynamic data for several fuels are also presented (p. 1)." @default.
- W1567380891 created "2016-06-24" @default.
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- W1567380891 date "1956-10-10" @default.
- W1567380891 modified "2023-09-27" @default.
- W1567380891 title "Methods for calculating thrust augmentation and liquid consumption for various turbojet-afterburner fuels" @default.
- W1567380891 hasPublicationYear "1956" @default.
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