The Application of Short-duration Techniques to the Experimental Study of Base Heating |
Common terms and phrases
ambient pressure APPLICATION OF SHORT-DURATION base heat transfer base heating problems base plate boundary layer Btu/ft2-sec calculated COMBUSTION CHAMBER constant pressure combustor CONSTANT VOLUME COMBUSTOR convective Cornell Aeronautical Laboratory diaphragm station DISTRIBUTION AT VARIOUS duplicated exhaust jets EXIT PLANE expansion wave external flow feet Figure four nozzles gages Gas Mixtures Goethert heat transfer rate high altitude hydrogen instrumentation jet spreading Liquid Oxygen lower altitudes milliseconds oscilloscope oxygen parameters PB/PR platinum film predicted pressure and heat PRESSURE BASE PRESSURE pressure transducers PSIA radiative heat transfer RATIO OF STAGNATION resistance thermometer ROCKET BASE rocket chamber pressure ROCKET NOZZLE EXIT SCHLIEREN shock tube shock waves short-duration flow SHORT-DURATION TECHNIQUES shown in Fig simulation Stagnation Point stagnation pressure stagnation region static pressure steady flow STUDY OF BASE tank temperature test chamber test period Theoretical Thermal Conductivity Tullahoma vacuum variation Viscosity volume combustion WADC wall enthalpy