Publisher's Synopsis
Several modifications have been made to the axial-flow turbine preliminary sizing code TURBAN. Turbine cooling has been added to the analysis. New alternative input options allow direct specification of stage reaction, stage work factor, and stage work split. The Reynolds number loss dependency was modified and an internal calculation of air viscosity was added. A complete description of input and output along with sample cases are included. Glassman, Arthur J. NASA-CR-195405, E-9252, NAS 1.26:195405 NAG3-1165; RTOP 505-69-50...
