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Input generator for Denton 3-dimensional turbomachine-blade-row analysis codeA users manual is presented for a computer program that prepares the bulk of the input data set required for the Denton three dimensional turbomachine blade row analysis code. The Denton input is generated from a minimum of geometry and flow variable information by using cubic spline curve fitting procedures. The features of the program are discussed. The input is described and special instructions are included to assist in its preparation. Sample input and output are included.
Document ID
19830018546
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Glassman, A. J. (NASA Lewis Research Center Cleveland, OH, United States)
Wood, J. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1983
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:83324
E-1565
NASA-TM-83324
Report Number: NAS 1.15:83324
Report Number: E-1565
Report Number: NASA-TM-83324
Accession Number
83N26817
Funding Number(s)
PROJECT: RTOP 505-31-0
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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