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Computer program for the design of axial-flow turbinesComputer program, capable of analyzing single and multispool units, computes absolute and relative flow fields within the turbine at the first stator inlet, at each interblade row plane, and at the final rotor exit. No simplifying assumptions are made which would result in restrictive design.
Document ID
19700000649
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Carter, A. F.
(NORTHERN RES. AND ENG. CORP.)
Lenherr, F. K.
Date Acquired
August 5, 2013
Publication Date
December 1, 1970
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LEW-11029
Report Number: LEW-11029
Accession Number
70B10669
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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