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AGARD ambient pressure APPLICATION OF SHORT-DUR base flow base heat transfer base heating problems base plate base region boundary layer Btu/ft^-sec calculated characteristic combustion chamber constant pressure combustor CONSTANT VOLUME COMBUSTOR convective convective heating Cornell Aeronautical Laboratory diaphragm station DISTRIBUTION AT VARIOUS duplicated exhaust jets external flow Fano feet Figure flow phenomena flow regimes gages Gas Mixtures Goethert heat flux heat transfer rates Hertzberg high altitudes iix3 initial pressure investigation jet spreading K. D. Bird J. W. Liquid Hydrogen Liquid Oxygen lower altitudes milliseconds NASA nozzle exit oxygen parameters predicted present tests pressure and heat pressure transducers psia radiative heat transfer ratio reverse flow rocket chamber pressure runs shock tube shock waves SHORT-DURATION TECHNIQUES shown in Fig simulation stagnation pressure stagnation region static pressure STUDY OF BASE tank temperature test chamber test period Theoretical theories Thermal Conductivity vacuum values variation VARIOUS ALTITUDES WADC wall enthalpy