high mass flow, ceramic ram jet burner |
Common terms and phrases
0.10 FUEL/AIR RATIO 120 Theoretical Maximum 15 inch long 18 inch 1950 Inside dia Adiabatic Flame Temperature Air Ratio air supply blowout BURNER Data obtained burner length calculated calibrated ceramic lined combustion ceramic surface temperature chamber cross-sectional area combustion chamber cross-sectional Combustion Chamber Parameter COMBUSTION PARAMETER COMBUSTION PARAMETER Sa conventional ramjet burners DEGREES F diameter equation exit gas exit Mach number exit pressure exit temperature experimental data flame holder Flameholder friction loss Fuel FUEL/AIR RATIO lbs heat high mass flows higher mass velocities inch long burner inlet pressure measurement lbs/sec lbs/sec/sq.ft Length 18 lined combustion chambers mass velocity ranges Massillon Refractories Company OPTICAL PYROMETER TEMP OPTICAL PYROMETER TEMPERATURE Phillips Petroleum Company PLOT OF OPTICAL pressure drop propane/lbs psia RATIO FOR 18 stagnation temperature stoichiometric stream thrust Test Stand Theoretical Adiabatic Flame University of Michigan UPSTREAM BURNER PRESSURE upstream pressure VALVE velocity of sound