Methods for calculating thrust augmentation and liquid consumption for various turbojet-afterburner fuels
Description: "Methods are presented 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).
Date: October 10, 1956
Creator: Morris, James F.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department