NASA TN D-3183
Stanley M. Nosek, Louis J. Goldman, Lewis Research Center, United States. National Aeronautics and Space Administration
National Aeronautics and Space Administration, 1966 - Aerodynamics - 19 pages
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9 pounds Alkali Metal approximately assumed calculated calibration curve coefficient of 0.97 Comparison condensate volumeter condenser temperature convergent-divergent nozzle Critical flow rates critical pressure ratios DATA Run Sepa demister derived from flow downstream effect of superheat equilibrium process expansion process experimental flows figure 6(a flow coefficient flow measurements flowmeter heat at constant heat Nozzle Condenser isentropic level probes manometer measured flows NASA TN Nozzle Condenser outlet nozzle inlet pressure nozzle inlet temperature nozzle throat nozzle were measured obeying pvn pansion indexes percent at pressures pounds per square pressure measurements pressure ratio measurements process expansion index properties from reference psia rator Super reference 9 research nozzle saturated conditions Saturated Vapor Saturated Vapor Pressure saturation temperature separator temperature shown in figure Sodium Vapor specific heat specific volume square inch absolute supersaturated process supersaturated-equilibrium process supersaturated-frozen process swirler temperature was measured thermocouple Thermodynamic Properties throat pressure upstream Vapor flow rate w/At weight flow