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Extended parametric representation of compressor fans and turbines. Volume 2: Part user's manual (parametric turbine)A turbine modeling technique has been developed which will enable the user to obtain consistent and rapid off-design performance from design point input. This technique is applicable to both axial and radial flow turbine with flow sizes ranging from about one pound per second to several hundred pounds per second. The axial flow turbines may or may not include variable geometry in the first stage nozzle. A user-specified option will also permit the calculation of design point cooling flow levels and corresponding changes in efficiency for the axial flow turbines. The modeling technique has been incorporated into a time-sharing program in order to facilitate its use. Because this report contains a description of the input output data, values of typical inputs, and example cases, it is suitable as a user's manual. This report is the second of a three volume set. The titles of the three volumes are as follows: (1) Volume 1 CMGEN USER's Manual (Parametric Compressor Generator); (2) Volume 2 PART USER's Manual (Parametric Turbine); (3) Volume 3 MODFAN USER's Manual (Parametric Modulation Flow Fan).
Document ID
19860014466
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Coverse, G. L.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1984
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-174646
NAS 1.26:174646
R84AEB379-VOL-2
Report Number: NASA-CR-174646
Report Number: NAS 1.26:174646
Report Number: R84AEB379-VOL-2
Accession Number
86N23937
Funding Number(s)
CONTRACT_GRANT: NAS3-23055
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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