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A Literature Survey G P Button
The Effects of Several Variables Upon the Ignition Lag of Hypergolic Fuels Oxidized
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adiabatic Aero aerodynamic Aerojet Aeronautical Air Force Aircraft altitude American Rocket Society atmosphere Aviation British Interplanetary Society burning program calculated California Institute cavitating cent Chem chemical coefficient combustion chamber constant coolant cooling cosmic density developed effect energy enthalpy Equation Experimental flame flight flow fluid frequency fuel function furfuryl alcohol gases Guided Missiles heat transfer hydrogen peroxide ignition lag impingement initial injection injector head Institute of Technology Interplanetary isentropic isothermal expansion jet engine Jet Propulsion Journal Laboratory liquid hydrogen mass maximum mixture ratio nozzle obtained operation optimum oscillations oxidizer oxygen paper Phys power plant present pressure ratio problem propellant psia Purdue University radiation ramjet range reaction Research rocket engine rocket motor Rocket Power Section solution space specific impulse spray stability Supersonic temperature thermal thrust chamber tion turbojet unit unsigned values valve vapor vehicle velocity weight WFNA