Effect of Heat-Capacity Lag on a Variety of Turbine-Nozzle Flow Processes
Description:
Note presenting the computation of the effect of heat-capacity lag in the adiabatic expansion of a gas through a turbine nozzle computed using a one-dimensional analysis of a representative flow process. A number of parameter variations in the flow process are considered to determine the factors that amplify this effect and to show the magnitude of the deviation from equilibrium conditions.
Date:
October 1950
Creator:
Spooner, Robert B.
Item Type:
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Partner:
UNT Libraries Government Documents Department