National Aeronautics and Space Administration (NASA)
Published: 2018-07-15
Total Pages: 30
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Computer code TD2 computes design point velocity diagrams and performance for multistage, multishaft, cooled or uncooled, axial flow turbines. This streamline analysis code was recently modified to upgrade modeling related to turbine cooling and to the internal loss correlation. These modifications are presented in this report along with descriptions of the code's expanded input and output. This report serves as the users manual for the upgraded code, which is named TD2-2. Glassman, Arthur J. Unspecified Center NAG3-1165; RTOP 505-69-50...