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Users manual and modeling improvements for axial turbine design and performance computer code TD2-2Computer 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.
Document ID
19920018133
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Glassman, Arthur J.
(Toledo Univ. OH, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:189118
NASA-CR-189118
E-6828
Report Number: NAS 1.26:189118
Report Number: NASA-CR-189118
Report Number: E-6828
Accession Number
92N27376
Funding Number(s)
CONTRACT_GRANT: NAG3-1165
PROJECT: RTOP 505-69-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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